ORBITIQ Sentinel V3 — Mission Operations Center

LIVE ORBITAL AWARENESS

4 THREATS

SPACE WEATHER

MODERATE

187

SOLAR FLUX (SFU)

Kp 4.2

GEOMAGNETIC

STORM LEVEL

+12%

DRAG INCREASE

AI IMPACT ASSESSMENT

Elevated solar flux causing 12% atmospheric drag increase at 400km. Orbit decay acceleration: 8m/day above baseline. Radiation belt enhancement may affect GEO assets. Recommend orbit correction planning within 72 hours.

AI MISSION STATUS — ORBITIQ-DEMO-01

ATTENTION REQUIRED

ORBITIQ-DEMO-01

OPERATIONAL — DEGRADED

POWER HEALTH

24% CRITICAL

COMMUNICATIONS

NOMINAL

THERMAL

STABLE

PROPULSION

DEGRADING

MISSION IMPACT

MODERATE

PRED FAILURE

18 ± 3 DAYS

AI REASONING — CONFIDENCE 94%

Battery internal resistance increased 340% over 72h, consistent with accelerated Li-ion degradation under thermal cycling. Solar panel output declining at 0.8%/day. Recommend immediate power budget review and payload duty cycle reduction. Conjunction risk with DEBRIS-66721 in 2.6 days adds operational pressure.

DIGITAL TWIN

CONJUNCTION RISK & MISSION TIMELINE

CONJUNCTIONS

TIMELINE

AI ARCH

STARLINK-7218vsDEBRIS-66721

HIGH RISK

2d 14h

TCA

420 m

MISS DIST

1.8E-4

› RECOMMENDED: 0.32 m/s radial burn at T-36h

ORBITIQ-DEMO-01vsDEBRIS-66721

HIGH RISK

2d 19h

TCA

380 m

MISS DIST

2.1E-4

› RECOMMENDED: 0.41 m/s radial burn at T-48h · Evaluate power budget first

NAVIC-1FvsSL-16 R/B

MEDIUM

6d 2h

TCA

1.4 km

MISS DIST

3.2E-5

› MONITOR: Update CDM in 48h. No maneuver required at current Pc.

IRNSS-1GvsCOSMOS-2251 DEB

LOW

9d 7h

TCA

4.2 km

MISS DIST

8.1E-6

› ROUTINE MONITORING. No action required.

24H

30D

REAL-TIME AI DATA FLOW — ORBITIQ-DEMO-01

Telemetry Ingestion (18 params · 1 Hz)

↓

Feature Engineering · Normalization · Windowing (60s)

↓

LSTM Autoencoder · Reconstruction Error

↓

Anomaly Detection · Severity 0–100 · F1=0.984

↓

Root Cause Analysis · SHAP Attribution

↓

Digital Twin · Subsystem Simulation

↓

Recommendation Engine · LLM Reasoning

↓

Mission Operator Decision Support

PREDICTIVE MAINTENANCE

3 CRITICAL

Power

24%

18d

Comms

53%

41d

Attitude

58%

55d

Propulsion

54%

48d

Thermal

78%

90d

Reaction Wheel #2

▼ DEGRADING

61%

HEALTH

78%

FAIL PROB

24d

RUL

› Reduce spin-up frequency. Inspect bearing assembly.

Battery Cell Array

▼ CRITICAL

24%

HEALTH

91%

FAIL PROB

18d

RUL

› Enable balancing mode. Reduce payload duty cycle 15%.

Thruster Valve #1

▼ WARNING

47%

HEALTH

52%

FAIL PROB

36d

RUL

› Monitor propellant flow rate. Schedule valve inspection.

ROOT CAUSE INTELLIGENCE

CONF 96%

PRIMARY Battery Internal Resistance +340%

SECONDARY Solar Panel Output −18%

Thermal Cycling Radiation Exposure Eclipse Duration ↑ Overcharge Events

battery_soc

82%

bus_voltage

61%

solar_current

45%

battery_temp

33%

panel_temp

21%

LSTM reconstruction error: 0.0428 (threshold: 0.0156) · SHAP confidence: 96%

CAUSAL CHAIN

Solar Flux +187 SFU

↓

Power Fluctuation → Overcharge

↓

Battery Cell Stress → IR ↑340%

↓

Thermal Increase → Cycling

↓

Comms Efficiency −4%

AUTONOMOUS RECOMMENDATIONS

12 ACTIVE

ALERT #A1298 · PRIORITY HIGH

IMMEDIATE

Power consumption anomaly — battery degradation

Battery cell array at 24% health, 91% failure probability. Reduce payload duty cycle immediately to preserve remaining capacity.

Reduce payload duty cycle by 15%

Enable battery balancing mode

Increase telemetry sampling to 10 Hz

Schedule maintenance review within 72h

ALERT #A1301 · PRIORITY HIGH

URGENT

Conjunction avoidance — DEBRIS-66721

Pc 2.1E-4 exceeds threshold. Avoidance maneuver required before T-48h window closes. Evaluate power budget before burn.

Execute 0.41 m/s radial burn at T-48h

Verify power budget pre-maneuver

Update CDM post-maneuver

ALERT #A1299 · PRIORITY MED

PLANNED

Reaction wheel #2 — bearing degradation

RW-2 bearing friction increased 28%. Schedule corrective action before 24-day RUL expires.

Reduce spin-up frequency by 30%

Switch primary attitude control to RW-1/3

Schedule ground maintenance window