STARLINK-37283, 68568
Orbit data source: Space-Track
STARLINK-37283, 68568 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 02 Apr 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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68568 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
RCS unknown
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 STARLINK-37283
1 68568U 26070AC 26145.60968955 .00030478 00000-0 90923-3 0 9992
2 68568 53.1591 5.1520 0001853 87.0017 273.1197 15.34409905 8336Epoch: 2026-05-25T14:37Z
TLE epoch observation values (Epoch: 2026-05-25T14:37:57.177Z)
Latitude
-0.00005°
Longitude
-97.5313°
Altitude
463.506 km
Speed
7.636 km/s
True Right ascension
00h 20m 36s
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
10:22:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.198 km
Perigee altitude
461.663 km
Semi-major axis
6,841.068 km
Eccentricity
0.00019
Inclination
53.1591°
RAAN
5.152°
Arg. of periapsis
87.0017°
True anomaly
273.0985°
Mean anomaly
273.1197°
Eccentric anomaly
273.1091°
Mean motion
3.83581 °/min
Orbital period
93.85 mins
BSTAR
0.00090923
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Other satellites on launch #70 in the year 2026 (2026-04-02 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-37283 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 | 2026-05-26 17:24:15.213Z | 237.352° WSW | 2026-05-26 17:26:15.213Z | 269.79° W | 42.566° | 2026-05-26 17:29:15.213Z | 45.414° ENE |
| 5 mins | 2026-05-26 23:58:15.213Z | 311.096° NW | 2026-05-27 00:00:15.213Z | 320.493° NNW | 44.081° | 2026-05-27 00:03:15.213Z | 129.719° 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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