STARLINK-32402, 61708
Orbit data source: Space-Track
STARLINK-32402, 61708 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 30 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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61708 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: 21 hours ago
TLE from 21 hours ago
0 STARLINK-32402
1 61708U 24196B 26270.19505185 .00000467 00000-0 24970-4 0 9998
2 61708 53.1583 242.1360 0001368 80.4468 279.6690 15.34380482108056Epoch: 2026-09-27T04:40Z
TLE epoch observation values (Epoch: 2026-09-27T04:40:52.479Z)
Latitude
0.00003°
Longitude
165.92511°
Altitude
463.505 km
Speed
7.636 km/s
True Right ascension
16h 08m 32s
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
19:11:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.954 km
Perigee altitude
462.083 km
Semi-major axis
6,841.155 km
Eccentricity
0.00014
Inclination
53.1583°
RAAN
242.136°
Arg. of periapsis
80.4468°
True anomaly
279.65355°
Mean anomaly
279.669°
Eccentric anomaly
279.66127°
Mean motion
3.83574 °/min
Orbital period
93.85 mins
BSTAR
0.00002497
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Other satellites on launch #196 in the year 2024 (2024-10-30 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-32402 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-28 02:50:55.187Z | 306.965° NW | 2026-09-28 02:52:55.187Z | 343.039° N | 15.627° | 2026-09-28 02:54:55.187Z | 17.595° NNE |
| 5 mins | 2026-09-28 06:07:55.187Z | 336.412° NNW | 2026-09-28 06:10:55.187Z | 31.486° NE | 18.406° | 2026-09-28 06:12:55.187Z | 66.707° ENE |
| 5 mins | 2026-09-28 07:46:55.187Z | 307.103° NW | 2026-09-28 07:48:55.187Z | 148.681° SSE | 70.741° | 2026-09-28 07:51:55.187Z | 133.54° SE |
| 6 mins | 2026-09-29 00:37:55.187Z | 231.362° WSW | 2026-09-29 00:40:55.187Z | 260.796° W | 78.727° | 2026-09-29 00:43:55.187Z | 48.242° ENE |
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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