STARLINK-32577, 62044
Orbit data source: Space-Track
STARLINK-32577, 62044 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 21 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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62044 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
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 STARLINK-32577
1 62044U 24216N 25256.49231625 .00018044 00000-0 66341-3 0 9993
2 62044 42.9961 184.1262 0001376 261.7150 98.3545 15.27589689 46703Epoch: 2025-09-13T11:48Z
TLE epoch observation values (Epoch: 2025-09-13T11:48:56.124Z)
Latitude
-0.00004°
Longitude
14.16741°
Altitude
482.932 km
Speed
7.626 km/s
True Right ascension
12h 16m 30s
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
01:59:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.91 km
Perigee altitude
484.022 km
Semi-major axis
6,863.103 km
Eccentricity
0.00014
Inclination
42.9961°
RAAN
184.1262°
Arg. of periapsis
261.715°
True anomaly
98.3701°
Mean anomaly
98.3545°
Eccentric anomaly
98.3623°
Mean motion
3.81735 °/min
Orbital period
94.31 mins
BSTAR
0.00066341
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Other satellites on launch #216 in the year 2024 (2024-11-21 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-32577 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 | 2025-09-14 22:34:44.233Z | 218.033° SW | 2025-09-14 22:36:44.233Z | 139.645° SSE | 37.664° | 2025-09-14 22:39:44.233Z | 79.26° E |
| 5 mins | 2025-09-15 00:13:44.233Z | 281.689° WNW | 2025-09-15 00:15:44.233Z | 12.786° NNE | 39.87° | 2025-09-15 00:18:44.233Z | 70.177° E |
| 5 mins | 2025-09-15 01:52:44.233Z | 297.448° NW | 2025-09-15 01:54:44.233Z | 13.253° NNE | 40.504° | 2025-09-15 01:57:44.233Z | 87.457° E |
| 5 mins | 2025-09-15 03:31:44.233Z | 271.326° WNW | 2025-09-15 03:33:44.233Z | 199.749° SSW | 37.83° | 2025-09-15 03:36:44.233Z | 132.028° 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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