STARLINK-36392, 68115
Orbit data source: Space-Track
STARLINK-36392, 68115 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Sun, 08 Mar 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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68115 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 17.7 m
Radar Cross Section
41.120 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 STARLINK-36392
1 68115U 26044Q 26246.82904372 .00016126 00000-0 50064-3 0 9996
2 68115 97.2858 206.0257 0002266 88.7059 271.4444 15.33451815 28885Epoch: 2026-09-03T19:53Z
TLE epoch observation values (Epoch: 2026-09-03T19:53:49.377Z)
Latitude
0.00005°
Longitude
-75.39165°
Altitude
468.596 km
Speed
7.632 km/s
True Right ascension
13h 44m 06s
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
01:42:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.016 km
Perigee altitude
460.916 km
Semi-major axis
6,840.603 km
Eccentricity
0.00023
Inclination
97.2858°
RAAN
206.0257°
Arg. of periapsis
88.7059°
True anomaly
271.41844°
Mean anomaly
271.4444°
Eccentric anomaly
271.43142°
Mean motion
3.8362 °/min
Orbital period
93.84 mins
BSTAR
0.00050064
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Other satellites on launch #44 in the year 2026 (2026-03-08 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-36392 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 | 2026-09-04 10:33:04.143Z | 356.262° N | 2026-09-04 10:36:04.143Z | 263.793° W | 35.389° | 2026-09-04 10:38:04.143Z | 216.335° SW |
| 5 mins | 2026-09-04 21:06:04.143Z | 137.392° SSE | 2026-09-04 21:08:04.143Z | 70.635° E | 35.102° | 2026-09-04 21:11:04.143Z | 2.493° NNE |
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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