STARLINK-32331, 61623
Orbit data source: Space-Track
STARLINK-32331, 61623 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 23 Oct 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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61623 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: 16 hours ago
TLE from 16 hours ago
0 STARLINK-32331
1 61623U 24191C 26275.16492529 .00010643 00000-0 39582-3 0 9999
2 61623 43.0031 71.9470 0001254 253.6768 106.3946 15.27572004109077Epoch: 2026-10-02T03:57Z
TLE epoch observation values (Epoch: 2026-10-02T03:57:29.545Z)
Latitude
0.00001°
Longitude
1.68311°
Altitude
483.092 km
Speed
7.626 km/s
True Right ascension
04h 47m 47s
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
13:53:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.878 km
Perigee altitude
484.157 km
Semi-major axis
6,863.155 km
Eccentricity
0.00013
Inclination
43.0031°
RAAN
71.947°
Arg. of periapsis
253.6768°
True anomaly
106.40838°
Mean anomaly
106.3946°
Eccentric anomaly
106.40149°
Mean motion
3.81731 °/min
Orbital period
94.31 mins
BSTAR
0.00039582
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Other satellites on launch #191 in the year 2024 (2024-10-23 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-32331 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 | 2026-10-02 20:09:31.281Z | 265.515° W | 2026-10-02 20:12:31.281Z | 207.881° SW | 23.204° | 2026-10-02 20:14:31.281Z | 168.728° S |
| 4 mins | 2026-10-03 13:07:31.281Z | 179.901° S | 2026-10-03 13:08:31.281Z | 155.917° SSE | 25.375° | 2026-10-03 13:11:31.281Z | 93.964° ESE |
| 5 mins | 2026-10-03 14:45:31.281Z | 256.149° W | 2026-10-03 14:47:31.281Z | 331.97° NNW | 82.828° | 2026-10-03 14:50:31.281Z | 70.47° E |
| 5 mins | 2026-10-03 16:24:31.281Z | 292.079° WNW | 2026-10-03 16:26:31.281Z | 348.356° N | 50.191° | 2026-10-03 16:29:31.281Z | 73.473° E |
| 6 mins | 2026-10-03 18:03:31.281Z | 289.404° WNW | 2026-10-03 18:05:31.281Z | 299.011° NW | 72.645° | 2026-10-03 18:09:31.281Z | 107.768° ESE |
| 5 mins | 2026-10-03 19:42:31.281Z | 256.879° W | 2026-10-03 19:44:31.281Z | 214.197° SW | 23.992° | 2026-10-03 19:47:31.281Z | 159.766° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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