STARLINK-37370, 68806
Orbit data source: Space-Track
STARLINK-37370, 68806 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Thu, 23 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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68806 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 shape, 14.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 STARLINK-37370
1 68806U 26089E 26171.41668980 .00062065 00000-0 19113-2 0 9998
2 68806 97.2856 18.4318 0002629 82.0997 280.4653 15.33405536 5970Epoch: 2026-06-20T10:00Z
TLE epoch observation values (Epoch: 2026-06-20T10:00:01.998Z)
Latitude
2.40722°
Longitude
-40.51438°
Altitude
468.166 km
Speed
7.633 km/s
True Right ascension
01h 12m 30s
True Declination
2° 23' 32"
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
07:23:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.402 km
Perigee altitude
460.805 km
Semi-major axis
6,840.74 km
Eccentricity
0.00026
Inclination
97.2856°
RAAN
18.4318°
Arg. of periapsis
82.0997°
True anomaly
280.43567°
Mean anomaly
280.4653°
Eccentric anomaly
280.45049°
Mean motion
3.83609 °/min
Orbital period
93.85 mins
BSTAR
0.0019113
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Other satellites on launch #89 in the year 2026 (2026-04-23 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-37370 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 | 2026-06-21 02:13:07.657Z | 35.394° NE | 2026-06-21 02:16:07.657Z | 113.38° SE | 28.486° | 2026-06-21 02:18:07.657Z | 157.989° S |
| 5 mins | 2026-06-21 14:19:07.657Z | 205.156° SW | 2026-06-21 14:21:07.657Z | 266.198° W | 30.888° | 2026-06-21 14:24:07.657Z | 330.219° 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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