STARLINK-37477, 68912
Orbit data source: Space-Track
STARLINK-37477, 68912 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Thu, 30 Apr 2026 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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68912 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational spacecraft
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 STARLINK-37477
1 68912U 26097T 26140.58335648 .00000100 00000-0 35006-5 0 9995
2 68912 97.2855 336.2934 0001832 111.6782 215.6350 15.49190215 4489Epoch: 2026-05-20T14:00Z
TLE epoch observation values (Epoch: 2026-05-20T14:00:01.999Z)
Latitude
-32.67581°
Longitude
-107.27847°
Altitude
432.525 km
Speed
7.65 km/s
True Right ascension
22h 43m 52s
True Declination
-32° 30' 44"
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
07:32:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
417.26 km
Perigee altitude
414.771 km
Semi-major axis
6,794.153 km
Eccentricity
0.00018
Inclination
97.2855°
RAAN
336.2934°
Arg. of periapsis
111.6782°
True anomaly
215.62277°
Mean anomaly
215.635°
Eccentric anomaly
215.62889°
Mean motion
3.87561 °/min
Orbital period
92.89 mins
BSTAR
0.0000035006
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Other satellites on launch #97 in the year 2026 (2026-04-30 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-37477 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 | 2026-05-21 01:33:17.232Z | 30.379° NE | 2026-05-21 01:36:17.232Z | 121.562° SE | 31.283° | 2026-05-21 01:38:17.232Z | 166.285° S |
| 5 mins | 2026-05-21 13:31:17.232Z | 196.983° SSW | 2026-05-21 13:34:17.232Z | 280.517° WNW | 28.443° | 2026-05-21 13:36:17.232Z | 325.089° NNW |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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