STARLINK-32336, 61004
Orbit data source: Space-Track
STARLINK-32336, 61004 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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61004 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: 11 hours ago
TLE from 11 hours ago
0 STARLINK-32336
1 61004U 24158Q 26252.10748145 -.00000169 00000-0 61269-5 0 9994
2 61004 53.1594 290.7219 0001069 96.5223 263.5902 15.34388720113770Epoch: 2026-09-09T02:34Z
TLE epoch observation values (Epoch: 2026-09-09T02:34:46.397Z)
Latitude
0.00004°
Longitude
-96.13568°
Altitude
463.72 km
Speed
7.636 km/s
True Right ascension
19h 22m 53s
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
05:39:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.725 km
Perigee altitude
462.262 km
Semi-major axis
6,841.131 km
Eccentricity
0.00011
Inclination
53.1594°
RAAN
290.7219°
Arg. of periapsis
96.5223°
True anomaly
263.57803°
Mean anomaly
263.5902°
Eccentric anomaly
263.58411°
Mean motion
3.83576 °/min
Orbital period
93.85 mins
BSTAR
0.0000061269
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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-32336 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 | 2026-09-10 05:21:20.118Z | 233.155° WSW | 2026-09-10 05:23:20.118Z | 357.785° N | 82.047° | 2026-09-10 05:26:20.118Z | 48.37° ENE |
| 4 mins | 2026-09-10 10:17:20.118Z | 347.899° N | 2026-09-10 10:19:20.118Z | 25.964° NE | 16.601° | 2026-09-10 10:21:20.118Z | 60.61° ENE |
| 5 mins | 2026-09-10 11:55:20.118Z | 316.505° NNW | 2026-09-10 11:57:20.118Z | 63.988° ENE | 75.427° | 2026-09-10 12:00:20.118Z | 125.293° 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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