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, 14.5 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 STARLINK-31869
1 60196U 24124P 25257.44905251 -.00000042 00000-0 10716-4 0 9992
2 60196 53.1613 61.0328 0001253 91.2672 268.8472 15.30191951 67310Epoch: 2025-09-14T10:46Z
TLE epoch observation values (Epoch: 2025-09-14T10:46:38.136Z)
Latitude
-0.00007°
Longitude
-94.29405°
Altitude
476.156 km
Speed
7.629 km/s
True Right ascension
04h 04m 07s
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
02:06:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.354 km
Perigee altitude
474.637 km
Semi-major axis
6,853.632 km
Eccentricity
0.00013
Inclination
53.1613°
RAAN
61.0328°
Arg. of periapsis
91.2672°
True anomaly
268.83284°
Mean anomaly
268.8472°
Eccentric anomaly
268.84002°
Mean motion
3.82527 °/min
Orbital period
94.11 mins
BSTAR
0.000010716
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-15 13:36:41.812Z | 228.97° WSW | 2025-09-15 13:39:41.812Z | 50.035° ENE | 44.058° | 2025-09-15 13:42:41.812Z | 50.062° ENE |
| 4 mins | 2025-09-15 18:33:41.812Z | 339.367° N | 2025-09-15 18:35:41.812Z | 12.903° NNE | 15.916° | 2025-09-15 18:37:41.812Z | 51.262° ENE |
| 5 mins | 2025-09-15 20:12:41.812Z | 318.049° NNW | 2025-09-15 20:14:41.812Z | 74.699° E | 43.434° | 2025-09-15 20:17:41.812Z | 124.296° SE |
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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