STARLINK-32282, 61006
Orbit data source: Space-Track
STARLINK-32282, 61006 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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61006 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, 17.7 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 STARLINK-32282
1 61006U 24158S 25286.47652663 -.00000426 00000-0 -22697-5 0 9990
2 61006 53.1619 29.2200 0001304 103.7466 256.3680 15.30190179 63117Epoch: 2025-10-13T11:26Z
TLE epoch observation values (Epoch: 2025-10-13T11:26:11.900Z)
Latitude
-0.00004°
Longitude
-164.60837°
Altitude
476.355 km
Speed
7.629 km/s
True Right ascension
01h 56m 52s
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
09:35:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.394 km
Perigee altitude
474.607 km
Semi-major axis
6,853.638 km
Eccentricity
0.00013
Inclination
53.1619°
RAAN
29.22°
Arg. of periapsis
103.7466°
True anomaly
256.35348°
Mean anomaly
256.368°
Eccentric anomaly
256.36074°
Mean motion
3.82526 °/min
Orbital period
94.11 mins
BSTAR
-0.0000022697
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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-32282 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 | 2025-10-14 16:08:30.447Z | 315.795° NNW | 2025-10-14 16:11:30.447Z | 18.55° NNE | 42.197° | 2025-10-14 16:14:30.447Z | 119.197° SE |
| 5 mins | 2025-10-15 09:05:30.447Z | 212.264° SW | 2025-10-15 09:07:30.447Z | 96.933° ESE | 41.418° | 2025-10-15 09:10:30.447Z | 55.098° ENE |
| 4 mins | 2025-10-15 10:43:30.447Z | 296.682° NW | 2025-10-15 10:45:30.447Z | 339.106° N | 19.754° | 2025-10-15 10:47:30.447Z | 18.336° NNE |
| 4 mins | 2025-10-15 14:01:30.447Z | 341.803° N | 2025-10-15 14:03:30.447Z | 15.365° NNE | 14.453° | 2025-10-15 14:05:30.447Z | 50.285° 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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