STARLINK-32639, 62153
Orbit data source: Space-Track
STARLINK-32639, 62153 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 30 Nov 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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62153 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: 17 hours ago
TLE from 17 hours ago
0 STARLINK-32639
1 62153U 24224Q 25346.56830430 .00031911 00000-0 11651-2 0 9991
2 62153 43.0007 290.3195 0001456 264.4769 95.5916 15.27553728 58997Epoch: 2025-12-12T13:38Z
TLE epoch observation values (Epoch: 2025-12-12T13:38:21.491Z)
Latitude
-0.00006°
Longitude
4.22183°
Altitude
483.001 km
Speed
7.626 km/s
True Right ascension
19h 21m 16s
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
05:23:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.072 km
Perigee altitude
484.074 km
Semi-major axis
6,863.21 km
Eccentricity
0.00015
Inclination
43.0007°
RAAN
290.3195°
Arg. of periapsis
264.4769°
True anomaly
95.6082°
Mean anomaly
95.5916°
Eccentric anomaly
95.5999°
Mean motion
3.81726 °/min
Orbital period
94.31 mins
BSTAR
0.0011651
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Other satellites on launch #224 in the year 2024 (2024-11-30 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-32639 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-13 22:47:14.394Z | 186.058° SSW | 2025-12-13 22:49:14.394Z | 145.952° SSE | 20.162° | 2025-12-13 22:51:14.394Z | 105.206° ESE |
| 6 mins | 2025-12-14 00:25:14.394Z | 249.218° W | 2025-12-14 00:28:14.394Z | 79.724° E | 43.62° | 2025-12-14 00:31:14.394Z | 72.274° E |
| 5 mins | 2025-12-14 02:05:14.394Z | 293.971° NW | 2025-12-14 02:07:14.394Z | 13.043° NNE | 37.695° | 2025-12-14 02:10:14.394Z | 74.288° E |
| 5 mins | 2025-12-14 03:44:14.394Z | 291.936° WNW | 2025-12-14 03:46:14.394Z | 31.553° NE | 44.497° | 2025-12-14 03:49:14.394Z | 103.151° ESE |
| 4 mins | 2025-12-14 05:23:14.394Z | 253.821° W | 2025-12-14 05:25:14.394Z | 202.469° SSW | 24.564° | 2025-12-14 05:27:14.394Z | 161.466° S |
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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