STARLINK-37388, 68860
Orbit data source: Space-Track
STARLINK-37388, 68860 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Sun, 26 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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68860 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: 13 hours ago
TLE from 13 hours ago
0 STARLINK-37388
1 68860U 26094X 26171.30526661 .00022903 00000-0 70947-3 0 9991
2 68860 97.2851 185.8165 0000478 81.8156 278.3141 15.33451037 8538Epoch: 2026-06-20T07:19Z
TLE epoch observation values (Epoch: 2026-06-20T07:19:35.035Z)
Latitude
0.00001°
Longitude
167.39872°
Altitude
468.59 km
Speed
7.632 km/s
True Right ascension
12h 23m 15s
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
07:15:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
462.795 km
Perigee altitude
462.141 km
Semi-major axis
6,840.605 km
Eccentricity
0.00005
Inclination
97.2851°
RAAN
185.8165°
Arg. of periapsis
81.8156°
True anomaly
278.30868°
Mean anomaly
278.3141°
Eccentric anomaly
278.31139°
Mean motion
3.8362 °/min
Orbital period
93.84 mins
BSTAR
0.00070947
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Other satellites on launch #94 in the year 2026 (2026-04-26 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-37388 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 00:41:13.085Z | 143.482° SSE | 2026-06-21 00:44:13.085Z | 59.803° ENE | 33.967° | 2026-06-21 00:47:13.085Z | 2.072° NNE |
| 5 mins | 2026-06-21 13:39:13.085Z | 25.291° NE | 2026-06-21 13:41:13.085Z | 78.261° E | 39.652° | 2026-06-21 13:44:13.085Z | 178.08° S |
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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