STARLINK-32846, 62867
Orbit data source: Space-Track
STARLINK-32846, 62867 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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62867 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: 8 hours ago
TLE from 8 hours ago
0 STARLINK-32846
1 62867U 25022P 25304.70741183 .00039440 00000-0 13381-2 0 9993
2 62867 53.1600 8.6184 0001293 65.7399 294.3736 15.30166679 42157Epoch: 2025-10-31T16:58Z
TLE epoch observation values (Epoch: 2025-10-31T16:58:40.382Z)
Latitude
-0.00006°
Longitude
73.70212°
Altitude
475.849 km
Speed
7.629 km/s
True Right ascension
00h 34m 28s
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
21:01:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.457 km
Perigee altitude
474.685 km
Semi-major axis
6,853.708 km
Eccentricity
0.00013
Inclination
53.16°
RAAN
8.6184°
Arg. of periapsis
65.7399°
True anomaly
294.3601°
Mean anomaly
294.3736°
Eccentric anomaly
294.36685°
Mean motion
3.82521 °/min
Orbital period
94.11 mins
BSTAR
0.0013381
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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-32846 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-01 07:16:52.986Z | 232.859° WSW | 2025-11-01 07:18:52.986Z | 252.968° W | 43.758° | 2025-11-01 07:21:52.986Z | 47.946° ENE |
| 4 mins | 2025-11-01 12:13:52.986Z | 344.602° N | 2025-11-01 12:15:52.986Z | 21.753° NNE | 16.667° | 2025-11-01 12:17:52.986Z | 58.485° ENE |
| 6 mins | 2025-11-01 13:51:52.986Z | 313.339° NW | 2025-11-01 13:53:52.986Z | 334.974° NNW | 43.165° | 2025-11-01 13:57:52.986Z | 127.595° 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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