STARLINK-11552, 62907
Orbit data source: Space-Track
STARLINK-11552, 62907 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 08 Feb 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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62907 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, 18.1 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 STARLINK-11552
1 62907U 25027A 26031.89261510 .00196399 00000-0 14912-2 0 9990
2 62907 43.0044 209.5800 0004807 283.2460 76.7871 15.70942229 57402Epoch: 2026-01-31T21:25Z
TLE epoch observation values (Epoch: 2026-01-31T21:25:21.944Z)
Latitude
-0.00006°
Longitude
117.12842°
Altitude
355.236 km
Speed
7.698 km/s
True Right ascension
13h 58m 19s
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
01:25:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
361.422 km
Perigee altitude
354.946 km
Semi-major axis
6,736.321 km
Eccentricity
0.00048
Inclination
43.0044°
RAAN
209.58°
Arg. of periapsis
283.246°
True anomaly
76.84073°
Mean anomaly
76.7871°
Eccentric anomaly
76.81392°
Mean motion
3.92563 °/min
Orbital period
91.71 mins
BSTAR
0.0014912
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Other satellites on launch #27 in the year 2025 (2025-02-08 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-11552 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 | 2026-02-02 14:50:24.078Z | 219.773° SW | 2026-02-02 14:52:24.078Z | 154.439° SSE | 33.428° | 2026-02-02 14:54:24.078Z | 87.808° E |
| 4 mins | 2026-02-02 18:03:24.078Z | 305.018° NW | 2026-02-02 18:04:24.078Z | 341.561° N | 35.333° | 2026-02-02 18:07:24.078Z | 83.366° E |
| 4 mins | 2026-02-02 19:39:24.078Z | 270.865° WNW | 2026-02-02 19:40:24.078Z | 239.349° WSW | 35.834° | 2026-02-02 19:43:24.078Z | 128.083° 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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