STARLINK-36868, 68120
Orbit data source: Space-Track
STARLINK-36868, 68120 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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68120 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: 13 hours ago
TLE from 13 hours ago
0 STARLINK-36868
1 68120U 26044V 26171.44549863 .00012604 00000-0 39173-3 0 9992
2 68120 97.2782 131.7467 0002262 71.4794 288.6694 15.33473089 17337Epoch: 2026-06-20T10:41Z
TLE epoch observation values (Epoch: 2026-06-20T10:41:31.081Z)
Latitude
-0.00008°
Longitude
62.70719°
Altitude
468.077 km
Speed
7.632 km/s
True Right ascension
08h 46m 59s
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
10:18:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.949 km
Perigee altitude
460.855 km
Semi-major axis
6,840.539 km
Eccentricity
0.00023
Inclination
97.2782°
RAAN
131.7467°
Arg. of periapsis
71.4794°
True anomaly
288.64484°
Mean anomaly
288.6694°
Eccentric anomaly
288.65712°
Mean motion
3.83626 °/min
Orbital period
93.84 mins
BSTAR
0.00039173
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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-36868 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 10:45:44.482Z | 328.795° NNW | 2026-06-21 10:46:44.482Z | 298.296° NW | 28.238° | 2026-06-21 10:49:44.482Z | 225.106° WSW |
| 4 mins | 2026-06-21 21:17:44.482Z | 150.495° SSE | 2026-06-21 21:19:44.482Z | 32.463° NE | 40.432° | 2026-06-21 21:21:44.482Z | 356.876° N |
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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