STARLINK-36984, 68168
Orbit data source: Space-Track
STARLINK-36984, 68168 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 14 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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68168 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: 10 hours ago
TLE from 10 hours ago
0 STARLINK-36984
1 68168U 26050B 26219.55513051 .00007459 00000-0 23161-3 0 9998
2 68168 53.1588 283.0129 0001323 77.5044 282.6107 15.34406308 23827Epoch: 2026-08-07T13:19Z
TLE epoch observation values (Epoch: 2026-08-07T13:19:23.276Z)
Latitude
0.00004°
Longitude
127.0868°
Altitude
463.388 km
Speed
7.636 km/s
True Right ascension
18h 52m 03s
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
13:26:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.847 km
Perigee altitude
462.036 km
Semi-major axis
6,841.079 km
Eccentricity
0.00013
Inclination
53.1588°
RAAN
283.0129°
Arg. of periapsis
77.5044°
True anomaly
282.5959°
Mean anomaly
282.6107°
Eccentric anomaly
282.6033°
Mean motion
3.8358 °/min
Orbital period
93.85 mins
BSTAR
0.00023161
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Other satellites on launch #50 in the year 2026 (2026-03-14 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-36984 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 | 2026-08-08 06:41:19.604Z | 210.533° SW | 2026-08-08 06:44:19.604Z | 121.882° SE | 38.537° | 2026-08-08 06:47:19.604Z | 59.484° ENE |
| 4 mins | 2026-08-08 08:20:19.604Z | 295.267° NW | 2026-08-08 08:22:19.604Z | 342.849° N | 21.094° | 2026-08-08 08:24:19.604Z | 21.808° NNE |
| 5 mins | 2026-08-08 13:16:19.604Z | 335.447° NNW | 2026-08-08 13:18:19.604Z | 53.073° ENE | 34.726° | 2026-08-08 13:21:19.604Z | 108.918° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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