STARLINK-32860, 62856
Orbit data source: Space-Track
STARLINK-32860, 62856 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 01 Feb 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62856 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
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 STARLINK-32860
1 62856U 25022C 25259.08614494 .00034239 00000-0 11622-2 0 9992
2 62856 53.1599 220.9052 0001356 91.9084 268.2072 15.30215758 35166Epoch: 2025-09-16T02:04Z
TLE epoch observation values (Epoch: 2025-09-16T02:04:02.922Z)
Latitude
-0.00004°
Longitude
-165.38851°
Altitude
476.097 km
Speed
7.629 km/s
True Right ascension
14h 43m 37s
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
07:38:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.354 km
Perigee altitude
474.495 km
Semi-major axis
6,853.561 km
Eccentricity
0.00014
Inclination
53.1599°
RAAN
220.9052°
Arg. of periapsis
91.9084°
True anomaly
268.19167°
Mean anomaly
268.2072°
Eccentric anomaly
268.19943°
Mean motion
3.82533 °/min
Orbital period
94.11 mins
BSTAR
0.0011622
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Other satellites on launch #22 in the year 2025 (2025-02-01 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-32860 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-17 00:10:57.741Z | 227.269° WSW | 2025-09-17 00:14:57.741Z | 59.598° ENE | 42.799° | 2025-09-17 00:17:57.741Z | 50.957° ENE |
| 4 mins | 2025-09-17 05:08:57.741Z | 341.756° N | 2025-09-17 05:10:57.741Z | 16.456° NNE | 15.726° | 2025-09-17 05:12:57.741Z | 53.339° ENE |
| 6 mins | 2025-09-17 06:46:57.741Z | 316.124° NNW | 2025-09-17 06:49:57.741Z | 85.199° E | 41.762° | 2025-09-17 06:52:57.741Z | 122.985° 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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