STARLINK-37066, 68081
Orbit data source: Space-Track
STARLINK-37066, 68081 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 04 Mar 2026 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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68081 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, 17.7 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 STARLINK-37066
1 68081U 26042N 26102.21025182 .00194669 00000-0 12467-2 0 9996
2 68081 53.1592 27.6098 0001052 84.6976 275.4164 15.75209126 7374Epoch: 2026-04-12T05:02Z
TLE epoch observation values (Epoch: 2026-04-12T05:02:45.757Z)
Latitude
-0.00003°
Longitude
111.50064°
Altitude
344.887 km
Speed
7.703 km/s
True Right ascension
01h 50m 26s
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
20:41:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
345.005 km
Perigee altitude
343.59 km
Semi-major axis
6,722.435 km
Eccentricity
0.00011
Inclination
53.1592°
RAAN
27.6098°
Arg. of periapsis
84.6976°
True anomaly
275.4044°
Mean anomaly
275.4164°
Eccentric anomaly
275.4104°
Mean motion
3.9378 °/min
Orbital period
91.42 mins
BSTAR
0.0012467
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Other satellites on launch #42 in the year 2026 (2026-03-04 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-37066 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 | 2026-04-12 21:59:22.582Z | 242.406° WSW | 2026-04-12 22:01:22.582Z | 285.911° WNW | 38.947° | 2026-04-12 22:04:22.582Z | 43.043° NE |
| 4 mins | 2026-04-13 04:23:22.582Z | 316.227° NNW | 2026-04-13 04:25:22.582Z | 104.676° ESE | 40.441° | 2026-04-13 04:27:22.582Z | 125.227° 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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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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