STARLINK-37160, 68282
Orbit data source: Space-Track
STARLINK-37160, 68282 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 19 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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68282 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
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 STARLINK-37160
1 68282U 26055W 26171.40053777 .00010983 00000-0 33565-3 0 9990
2 68282 53.1584 200.2332 0001337 67.2818 292.8326 15.34405064 15686Epoch: 2026-06-20T09:36Z
TLE epoch observation values (Epoch: 2026-06-20T09:36:46.463Z)
Latitude
0°
Longitude
147.42391°
Altitude
463.235 km
Speed
7.636 km/s
True Right ascension
13h 20m 55s
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
07:12:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.86 km
Perigee altitude
462.031 km
Semi-major axis
6,841.082 km
Eccentricity
0.00013
Inclination
53.1584°
RAAN
200.2332°
Arg. of periapsis
67.2818°
True anomaly
292.81848°
Mean anomaly
292.8326°
Eccentric anomaly
292.82554°
Mean motion
3.8358 °/min
Orbital period
93.85 mins
BSTAR
0.00033565
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Other satellites on launch #55 in the year 2026 (2026-03-19 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-37160 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 04:33:09.442Z | 222.207° SW | 2026-06-21 04:36:09.442Z | 88.345° E | 42.952° | 2026-06-21 04:39:09.442Z | 53.189° ENE |
| 5 mins | 2026-06-21 11:08:09.442Z | 326.76° NNW | 2026-06-21 11:10:09.442Z | 71.959° E | 39.669° | 2026-06-21 11:13:09.442Z | 118.524° 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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