STARLINK-33779, 63880
Orbit data source: Space-Track
STARLINK-33779, 63880 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 10 May 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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63880 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 STARLINK-33779
1 63880U 25094S 26171.45270727 -.00000366 00000-0 -22871-4 0 9997
2 63880 70.0032 335.4559 0002816 263.6645 96.4194 14.98313219 62598Epoch: 2026-06-20T10:51Z
TLE epoch observation values (Epoch: 2026-06-20T10:51:53.908Z)
Latitude
0.00005°
Longitude
-96.18582°
Altitude
574.751 km
Speed
7.574 km/s
True Right ascension
22h 21m 49s
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
08:33:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.012 km
Perigee altitude
568.099 km
Semi-major axis
6,948.193 km
Eccentricity
0.00028
Inclination
70.0032°
RAAN
335.4559°
Arg. of periapsis
263.6645°
True anomaly
96.45147°
Mean anomaly
96.4194°
Eccentric anomaly
96.43543°
Mean motion
3.74745 °/min
Orbital period
96.07 mins
BSTAR
-0.000022871
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Other satellites on launch #94 in the year 2025 (2025-05-10 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-33779 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-20 22:38:27.572Z | 317.813° NNW | 2026-06-20 22:42:27.572Z | 234.476° WSW | 31.081° | 2026-06-20 22:45:27.572Z | 185.265° SSW |
| 6 mins | 2026-06-21 12:39:27.572Z | 225.535° WSW | 2026-06-21 12:41:27.572Z | 267.523° W | 38.178° | 2026-06-21 12:45:27.572Z | 13.851° NNE |
| 5 mins | 2026-06-21 21:04:27.572Z | 22.2° NNE | 2026-06-21 21:06:27.572Z | 67.314° ENE | 23.527° | 2026-06-21 21:09:27.572Z | 114.418° 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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