STARLINK-32679, 62507
Orbit data source: Space-Track
STARLINK-32679, 62507 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 06 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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62507 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: 22 hours ago
TLE from 22 hours ago
0 STARLINK-32679
1 62507U 25003W 26170.93292765 .00016330 00000-0 60096-3 0 9996
2 62507 43.0016 71.9188 0002140 258.3251 101.7361 15.27616245 82304Epoch: 2026-06-19T22:23Z
TLE epoch observation values (Epoch: 2026-06-19T22:23:24.948Z)
Latitude
-0.00001°
Longitude
-172.08996°
Altitude
483.015 km
Speed
7.626 km/s
True Right ascension
04h 47m 40s
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
07:16:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.354 km
Perigee altitude
483.417 km
Semi-major axis
6,863.023 km
Eccentricity
0.00021
Inclination
43.0016°
RAAN
71.9188°
Arg. of periapsis
258.3251°
True anomaly
101.76011°
Mean anomaly
101.7361°
Eccentric anomaly
101.7481°
Mean motion
3.81742 °/min
Orbital period
94.3 mins
BSTAR
0.00060096
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Other satellites on launch #3 in the year 2025 (2025-01-06 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-32679 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 | 2026-06-20 20:34:03.679Z | 212.591° SW | 2026-06-20 20:37:03.679Z | 137.039° SSE | 30.332° | 2026-06-20 20:40:03.679Z | 83.359° E |
| 6 mins | 2026-06-20 22:13:03.679Z | 266.509° W | 2026-06-20 22:16:03.679Z | 35.301° NE | 40.469° | 2026-06-20 22:19:03.679Z | 70.382° E |
| 5 mins | 2026-06-20 23:53:03.679Z | 299.936° NW | 2026-06-20 23:55:03.679Z | 25.105° NE | 38.088° | 2026-06-20 23:58:03.679Z | 81.916° E |
| 5 mins | 2026-06-21 01:32:03.679Z | 279.543° WNW | 2026-06-21 01:34:03.679Z | 170.873° S | 42.685° | 2026-06-21 01:37:03.679Z | 119.662° SE |
| 5 mins | 2026-06-21 20:07:03.679Z | 202.122° SSW | 2026-06-21 20:09:03.679Z | 144.352° SSE | 30.163° | 2026-06-21 20:12:03.679Z | 84.941° E |
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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