STARLINK-11529, 62599
Orbit data source: Space-Track
STARLINK-11529, 62599 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 13 Jan 2025 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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62599 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 V2MD, Unknown motor
Mass
960 kg wet, ~910 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: 2 days ago
TLE from 2 days ago
0 STARLINK-11529
1 62599U 25008N 25257.94097233 .00180942 00000-0 13814-2 0 9997
2 62599 42.9982 105.5063 0003767 201.7859 158.2849 15.70865432 39653Epoch: 2025-09-14T22:35Z
TLE epoch observation values (Epoch: 2025-09-14T22:35:00.009Z)
Latitude
-0°
Longitude
132.6035°
Altitude
358.55 km
Speed
7.695 km/s
True Right ascension
07h 02m 01s
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
01:21:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
360.942 km
Perigee altitude
355.867 km
Semi-major axis
6,736.541 km
Eccentricity
0.00038
Inclination
42.9982°
RAAN
105.5063°
Arg. of periapsis
201.7859°
True anomaly
158.30086°
Mean anomaly
158.2849°
Eccentric anomaly
158.29288°
Mean motion
3.92543 °/min
Orbital period
91.71 mins
BSTAR
0.0013814
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Other satellites on launch #8 in the year 2025 (2025-01-13 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-11529 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 | 2025-09-17 16:24:01.682Z | 212.701° SW | 2025-09-17 16:26:01.682Z | 149.313° SSE | 29.734° | 2025-09-17 16:28:01.682Z | 90.368° ESE |
| 4 mins | 2025-09-17 19:37:01.682Z | 308.11° NW | 2025-09-17 19:38:01.682Z | 351.643° N | 35.292° | 2025-09-17 19:41:01.682Z | 81.484° E |
| 4 mins | 2025-09-17 21:13:01.682Z | 274.206° WNW | 2025-09-17 21:14:01.682Z | 237.671° WSW | 39.724° | 2025-09-17 21:17:01.682Z | 122.222° 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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