STARLINK-36822, 67909
Orbit data source: Space-Track
STARLINK-36822, 67909 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 22 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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67909 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: 17 hours ago
TLE from 17 hours ago
0 STARLINK-36822
1 67909U 26036F 26171.30371303 .00004640 00000-0 17799-3 0 9995
2 67909 43.0006 25.9297 0000789 280.6431 79.4332 15.27585062 19412Epoch: 2026-06-20T07:17Z
TLE epoch observation values (Epoch: 2026-06-20T07:17:20.805Z)
Latitude
-0.00002°
Longitude
8.07273°
Altitude
482.71 km
Speed
7.626 km/s
True Right ascension
01h 43m 43s
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
11:43:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.521 km
Perigee altitude
484.438 km
Semi-major axis
6,863.116 km
Eccentricity
0.00008
Inclination
43.0006°
RAAN
25.9297°
Arg. of periapsis
280.6431°
True anomaly
79.44209°
Mean anomaly
79.4332°
Eccentric anomaly
79.43764°
Mean motion
3.81734 °/min
Orbital period
94.31 mins
BSTAR
0.00017799
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Other satellites on launch #36 in the year 2026 (2026-02-22 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-36822 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 16:25:58.682Z | 173.012° S | 2026-06-21 16:27:58.682Z | 135.48° SSE | 15.893° | 2026-06-21 16:29:58.682Z | 102.822° ESE |
| 5 mins | 2026-06-21 18:03:58.682Z | 238.905° WSW | 2026-06-21 18:05:58.682Z | 182.613° SSW | 43.447° | 2026-06-21 18:08:58.682Z | 75.297° E |
| 5 mins | 2026-06-21 19:42:58.682Z | 285.314° WNW | 2026-06-21 19:44:58.682Z | 340.298° N | 38.215° | 2026-06-21 19:47:58.682Z | 69.781° E |
| 6 mins | 2026-06-21 21:21:58.682Z | 292.733° NW | 2026-06-21 21:23:58.682Z | 327.586° NNW | 41.344° | 2026-06-21 21:27:58.682Z | 97.727° ESE |
| 5 mins | 2026-06-21 23:00:58.682Z | 266.675° W | 2026-06-21 23:02:58.682Z | 219.45° SW | 29.635° | 2026-06-21 23:05:58.682Z | 148.232° 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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