STARLINK-33887, 63680
Orbit data source: Space-Track
STARLINK-33887, 63680 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 28 Apr 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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63680 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: 15 hours ago
TLE from 15 hours ago
0 STARLINK-33887
1 63680U 25085S 26171.33678823 .00008849 00000-0 33060-3 0 9994
2 63680 42.9995 170.7687 0001569 264.9316 95.1357 15.27592300 64634Epoch: 2026-06-20T08:04Z
TLE epoch observation values (Epoch: 2026-06-20T08:04:58.503Z)
Latitude
0.00003°
Longitude
140.9721°
Altitude
482.884 km
Speed
7.626 km/s
True Right ascension
11h 23m 04s
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
10:18:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.034 km
Perigee altitude
483.881 km
Semi-major axis
6,863.095 km
Eccentricity
0.00016
Inclination
42.9995°
RAAN
170.7687°
Arg. of periapsis
264.9316°
True anomaly
95.15361°
Mean anomaly
95.1357°
Eccentric anomaly
95.14465°
Mean motion
3.81736 °/min
Orbital period
94.31 mins
BSTAR
0.0003306
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Other satellites on launch #85 in the year 2025 (2025-04-28 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-33887 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 03:06:43.155Z | 213.795° SW | 2026-06-21 03:09:43.155Z | 153.66° SSE | 29.433° | 2026-06-21 03:12:43.155Z | 87.347° E |
| 5 mins | 2026-06-21 04:46:43.155Z | 267.478° W | 2026-06-21 04:48:43.155Z | 358.379° N | 43.19° | 2026-06-21 04:51:43.155Z | 69.497° E |
| 5 mins | 2026-06-21 06:25:43.155Z | 294.998° NW | 2026-06-21 06:27:43.155Z | 356.249° N | 38.45° | 2026-06-21 06:30:43.155Z | 78.898° E |
| 5 mins | 2026-06-21 08:04:43.155Z | 283.189° WNW | 2026-06-21 08:06:43.155Z | 232.654° WSW | 43.494° | 2026-06-21 08:09:43.155Z | 118.414° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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