STARLINK-31954, 60102
Orbit data source: Space-Track
STARLINK-31954, 60102 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 23 Jun 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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60102 intel report (Beta)
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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: 1 day ago
TLE from 1 day ago
0 STARLINK-31954
1 60102U 24117M 26170.58009536 -.00007374 00000-0 -23675-3 0 9995
2 60102 53.1615 284.0502 0001195 99.9975 260.1161 15.30242571112480Epoch: 2026-06-19T13:55Z
TLE epoch observation values (Epoch: 2026-06-19T13:55:20.239Z)
Latitude
0.00002°
Longitude
167.40885°
Altitude
476.129 km
Speed
7.629 km/s
True Right ascension
18h 56m 12s
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
07:11:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.163 km
Perigee altitude
474.525 km
Semi-major axis
6,853.481 km
Eccentricity
0.00012
Inclination
53.1615°
RAAN
284.0502°
Arg. of periapsis
99.9975°
True anomaly
260.10261°
Mean anomaly
260.1161°
Eccentric anomaly
260.10935°
Mean motion
3.8254 °/min
Orbital period
94.11 mins
BSTAR
-0.00023675
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Other satellites on launch #117 in the year 2024 (2024-06-23 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-31954 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 | 2026-06-21 10:00:10.435Z | 232.495° WSW | 2026-06-21 10:03:10.435Z | 31.457° NE | 43.132° | 2026-06-21 10:06:10.435Z | 48.572° ENE |
| 4 mins | 2026-06-21 14:57:10.435Z | 340.224° N | 2026-06-21 14:59:10.435Z | 14.834° NNE | 16.543° | 2026-06-21 15:01:10.435Z | 53.717° ENE |
| 5 mins | 2026-06-21 16:36:10.435Z | 315.042° NNW | 2026-06-21 16:38:10.435Z | 101.708° ESE | 43.495° | 2026-06-21 16:41:10.435Z | 127.334° 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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