STARLINK-36969, 68167
Orbit data source: Space-Track
STARLINK-36969, 68167 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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68167 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: 19 hours ago
TLE from 19 hours ago
0 STARLINK-36969
1 68167U 26050A 26219.17062618 .00009794 00000-0 30062-3 0 9995
2 68167 53.1570 284.8712 0001756 45.1815 314.9330 15.34400774 23762Epoch: 2026-08-07T04:05Z
TLE epoch observation values (Epoch: 2026-08-07T04:05:42.101Z)
Latitude
-0.00005°
Longitude
-92.25442°
Altitude
462.754 km
Speed
7.637 km/s
True Right ascension
18h 59m 29s
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
13:25:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.16 km
Perigee altitude
461.757 km
Semi-major axis
6,841.095 km
Eccentricity
0.00018
Inclination
53.157°
RAAN
284.8712°
Arg. of periapsis
45.1815°
True anomaly
314.91875°
Mean anomaly
314.933°
Eccentric anomaly
314.92588°
Mean motion
3.83579 °/min
Orbital period
93.85 mins
BSTAR
0.00030062
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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-36969 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-08 06:50:05.607Z | 219.746° SW | 2026-08-08 06:53:05.607Z | 183.894° SSW | 40.422° | 2026-08-08 06:57:05.607Z | 54.812° ENE |
| 4 mins | 2026-08-08 08:30:05.607Z | 304.142° NW | 2026-08-08 08:31:05.607Z | 325.698° NNW | 19.105° | 2026-08-08 08:34:05.607Z | 24.114° NE |
| 5 mins | 2026-08-08 13:25:05.607Z | 323.14° NNW | 2026-08-08 13:27:05.607Z | 10.045° NNE | 38.106° | 2026-08-08 13:30:05.607Z | 111.665° 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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