STARLINK-32710, 62604
Orbit data source: Space-Track
STARLINK-32710, 62604 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 13 Jan 2025 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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62604 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: 2 days ago
TLE from 2 days ago
0 STARLINK-32710
1 62604U 25008T 25259.46998496 .00030907 00000-0 11263-2 0 9995
2 62604 42.9985 181.4778 0003169 277.1695 82.8796 15.27626643 38923Epoch: 2025-09-16T11:16Z
TLE epoch observation values (Epoch: 2025-09-16T11:16:46.7Z)
Latitude
-0.00004°
Longitude
16.62335°
Altitude
482.416 km
Speed
7.626 km/s
True Right ascension
12h 05m 54s
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
23:33:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
487.03 km
Perigee altitude
482.68 km
Semi-major axis
6,862.992 km
Eccentricity
0.00032
Inclination
42.9985°
RAAN
181.4778°
Arg. of periapsis
277.1695°
True anomaly
82.91564°
Mean anomaly
82.8796°
Eccentric anomaly
82.89762°
Mean motion
3.81745 °/min
Orbital period
94.3 mins
BSTAR
0.0011263
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Other satellites on launch #8 in the year 2025 (2025-01-13 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-32710 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-18 21:33:12.773Z | 219.149° SW | 2025-09-18 21:36:12.773Z | 137.869° SSE | 33.826° | 2025-09-18 21:39:12.773Z | 81.402° E |
| 6 mins | 2025-09-18 23:12:12.773Z | 270.464° WNW | 2025-09-18 23:15:12.773Z | 24.753° NE | 40.212° | 2025-09-18 23:18:12.773Z | 70.219° E |
| 5 mins | 2025-09-19 00:52:12.773Z | 299.125° NW | 2025-09-19 00:54:12.773Z | 21.761° NNE | 39.168° | 2025-09-19 00:57:12.773Z | 84.406° E |
| 5 mins | 2025-09-19 02:31:12.773Z | 275.24° WNW | 2025-09-19 02:33:12.773Z | 186.17° SSW | 40.788° | 2025-09-19 02:36:12.773Z | 125.244° 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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