STARLINK-32279, 61003
Orbit data source: Space-Track
STARLINK-32279, 61003 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 05 Sep 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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61003 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: 14 hours ago
TLE from 14 hours ago
0 STARLINK-32279
1 61003U 24158P 25260.10308864 -.00000664 00000-0 -10294-4 0 9993
2 61003 53.1607 151.8724 0001611 96.6894 263.4290 15.30179610 59073Epoch: 2025-09-17T02:28Z
TLE epoch observation values (Epoch: 2025-09-17T02:28:26.858Z)
Latitude
-0.00004°
Longitude
118.47662°
Altitude
476.302 km
Speed
7.629 km/s
True Right ascension
10h 07m 29s
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
09:02:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.636 km
Perigee altitude
474.428 km
Semi-major axis
6,853.669 km
Eccentricity
0.00016
Inclination
53.1607°
RAAN
151.8724°
Arg. of periapsis
96.6894°
True anomaly
263.41066°
Mean anomaly
263.429°
Eccentric anomaly
263.41983°
Mean motion
3.82524 °/min
Orbital period
94.11 mins
BSTAR
-0.000010294
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Other satellites on launch #158 in the year 2024 (2024-09-05 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-32279 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 | 2025-09-17 19:55:20.082Z | 244.887° WSW | 2025-09-17 19:57:20.082Z | 298.922° NW | 41.493° | 2025-09-17 20:00:20.082Z | 42.279° NE |
| 4 mins | 2025-09-18 00:52:20.082Z | 343.968° N | 2025-09-18 00:54:20.082Z | 23.353° NE | 18.691° | 2025-09-18 00:56:20.082Z | 62.963° ENE |
| 5 mins | 2025-09-18 02:30:20.082Z | 305.46° NW | 2025-09-18 02:32:20.082Z | 271.504° WNW | 43.412° | 2025-09-18 02:35:20.082Z | 137.061° SSE |
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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