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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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: 20 hours ago
TLE from 20 hours ago
0 STARLINK-32282
1 61006U 24158S 26304.55460511 .00039958 00000-0 11851-2 0 9997
2 61006 53.1608 45.6801 0001985 81.6567 278.4661 15.34461623121821Epoch: 2026-10-31T13:18Z
TLE epoch observation values (Epoch: 2026-10-31T13:18:37.881Z)
Latitude
0.00001°
Longitude
166.16361°
Altitude
463.222 km
Speed
7.636 km/s
True Right ascension
03h 02m 43s
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
04:31:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.135 km
Perigee altitude
461.419 km
Semi-major axis
6,840.914 km
Eccentricity
0.0002
Inclination
53.1608°
RAAN
45.6801°
Arg. of periapsis
81.6567°
True anomaly
278.4436°
Mean anomaly
278.4661°
Eccentric anomaly
278.45485°
Mean motion
3.83594 °/min
Orbital period
93.85 mins
BSTAR
0.0011851
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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 | 2026-11-01 09:49:36.017Z | 240.572° WSW | 2026-11-01 09:52:36.017Z | 2.89° NNE | 61.151° | 2026-11-01 09:55:36.017Z | 45.057° ENE |
| 5 mins | 2026-11-01 14:45:36.017Z | 337.61° N | 2026-11-01 14:48:36.017Z | 33.426° NE | 17.989° | 2026-11-01 14:50:36.017Z | 67.48° ENE |
| 6 mins | 2026-11-01 16:23:36.017Z | 308.955° NW | 2026-11-01 16:26:36.017Z | 140.138° SSE | 66.342° | 2026-11-01 16:29:36.017Z | 132.697° 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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