STARLINK-31869, 60196
Orbit data source: Space-Track
STARLINK-31869, 60196 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 03 Jul 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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60196 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 STARLINK-31869
1 60196U 24124P 25310.35401406 .00000436 00000-0 26837-4 0 9992
2 60196 53.1623 175.2950 0001288 89.9582 270.1567 15.30194135 75410Epoch: 2025-11-06T08:29Z
TLE epoch observation values (Epoch: 2025-11-06T08:29:46.814Z)
Latitude
0.00001°
Longitude
2.03641°
Altitude
476.13 km
Speed
7.629 km/s
True Right ascension
11h 41m 10s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
17:57:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.371 km
Perigee altitude
474.606 km
Semi-major axis
6,853.626 km
Eccentricity
0.00013
Inclination
53.1623°
RAAN
175.295°
Arg. of periapsis
89.9582°
True anomaly
270.14194°
Mean anomaly
270.1567°
Eccentric anomaly
270.14932°
Mean motion
3.82527 °/min
Orbital period
94.11 mins
BSTAR
0.000026837
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Other satellites on launch #124 in the year 2024 (2024-07-03 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.STARLINK-31869 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-07 22:33:18.298Z | 344.799° N | 2025-11-07 22:35:18.298Z | 20.861° NNE | 15.632° | 2025-11-07 22:37:18.298Z | 56.144° ENE |
| 6 mins | 2025-11-08 00:11:18.298Z | 317.426° NNW | 2025-11-08 00:13:18.298Z | 353.47° N | 41.447° | 2025-11-08 00:17:18.298Z | 122.722° SE |
| 5 mins | 2025-11-08 17:07:18.298Z | 216.467° SW | 2025-11-08 17:09:18.298Z | 115.726° SE | 43.235° | 2025-11-08 17:12:18.298Z | 54.64° ENE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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