STARLINK-32616, 61920
Orbit data source: Space-Track
STARLINK-32616, 61920 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 11 Nov 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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61920 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: 10 hours ago
TLE from 10 hours ago
0 STARLINK-32616
1 61920U 24207J 25312.86986986 .00044542 00000-0 16178-2 0 9990
2 61920 43.0020 244.1256 0001397 263.3211 96.7482 15.27591144 56243Epoch: 2025-11-08T20:52Z
TLE epoch observation values (Epoch: 2025-11-08T20:52:36.755Z)
Latitude
-0.00002°
Longitude
-117.32085°
Altitude
482.904 km
Speed
7.626 km/s
True Right ascension
16h 16m 30s
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
03:00:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.919 km
Perigee altitude
484.002 km
Semi-major axis
6,863.098 km
Eccentricity
0.00014
Inclination
43.002°
RAAN
244.1256°
Arg. of periapsis
263.3211°
True anomaly
96.7641°
Mean anomaly
96.7482°
Eccentric anomaly
96.75615°
Mean motion
3.81736 °/min
Orbital period
94.31 mins
BSTAR
0.0016178
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Other satellites on launch #207 in the year 2024 (2024-11-11 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-32616 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 | 2025-11-09 22:10:38.770Z | 193.778° SSW | 2025-11-09 22:12:38.770Z | 155.55° SSE | 21.792° | 2025-11-09 22:15:38.770Z | 95.307° ESE |
| 5 mins | 2025-11-09 23:49:38.770Z | 253.306° W | 2025-11-09 23:51:38.770Z | 325.223° NNW | 44.956° | 2025-11-09 23:54:38.770Z | 71.371° E |
| 5 mins | 2025-11-10 01:28:38.770Z | 291.16° WNW | 2025-11-10 01:30:38.770Z | 349.378° N | 37.799° | 2025-11-10 01:33:38.770Z | 73.451° E |
| 6 mins | 2025-11-10 03:07:38.770Z | 289.628° WNW | 2025-11-10 03:09:38.770Z | 305.457° NW | 43.828° | 2025-11-10 03:13:38.770Z | 106.659° ESE |
| 5 mins | 2025-11-10 04:46:38.770Z | 257.078° W | 2025-11-10 04:48:38.770Z | 212.983° SW | 22.832° | 2025-11-10 04:51:38.770Z | 157.988° S |
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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