STARLINK-36779, 67869
Orbit data source: Space-Track
STARLINK-36779, 67869 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 20 Feb 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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67869 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 + 2 Pan, 17.7 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 STARLINK-36779
1 67869U 26034V 26171.18175604 .00023341 00000-0 69895-3 0 9993
2 67869 53.1572 85.6275 0001266 88.9871 271.1277 15.34437981 19754Epoch: 2026-06-20T04:21Z
TLE epoch observation values (Epoch: 2026-06-20T04:21:43.721Z)
Latitude
-0.00001°
Longitude
111.79526°
Altitude
463.474 km
Speed
7.636 km/s
True Right ascension
05h 42m 30s
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
07:16:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.714 km
Perigee altitude
461.982 km
Semi-major axis
6,840.985 km
Eccentricity
0.00013
Inclination
53.1572°
RAAN
85.6275°
Arg. of periapsis
88.9871°
True anomaly
271.1132°
Mean anomaly
271.1277°
Eccentric anomaly
271.12045°
Mean motion
3.83588 °/min
Orbital period
93.85 mins
BSTAR
0.00069895
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Other satellites on launch #34 in the year 2026 (2026-02-20 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-36779 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 | 2026-06-20 21:45:48.844Z | 257.531° W | 2026-06-20 21:48:48.844Z | 321.387° NNW | 32.079° | 2026-06-20 21:51:48.844Z | 34.165° NE |
| 4 mins | 2026-06-21 02:43:48.844Z | 357.161° N | 2026-06-21 02:44:48.844Z | 23.582° NE | 23.371° | 2026-06-21 02:47:48.844Z | 84.834° E |
| 5 mins | 2026-06-21 04:20:48.844Z | 286.465° WNW | 2026-06-21 04:22:48.844Z | 220.225° SW | 34.648° | 2026-06-21 04:25:48.844Z | 154.426° SSE |
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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