STARLINK-36814, 67904
Orbit data source: Space-Track
STARLINK-36814, 67904 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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67904 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
RCS unknown
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 STARLINK-36814
1 67904U 26036A 26103.85433151 .00012518 00000-0 45188-3 0 9991
2 67904 43.0037 47.2516 0002910 277.0690 82.9831 15.28424669 9099Epoch: 2026-04-13T20:30Z
TLE epoch observation values (Epoch: 2026-04-13T20:30:14.242Z)
Latitude
-0.00002°
Longitude
-102.34672°
Altitude
480.054 km
Speed
7.628 km/s
True Right ascension
03h 09m 00s
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
15:06:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
484.463 km
Perigee altitude
480.47 km
Semi-major axis
6,860.603 km
Eccentricity
0.00029
Inclination
43.0037°
RAAN
47.2516°
Arg. of periapsis
277.069°
True anomaly
83.0162°
Mean anomaly
82.9831°
Eccentric anomaly
82.99965°
Mean motion
3.81944 °/min
Orbital period
94.25 mins
BSTAR
0.00045188
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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-36814 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 | 2026-04-14 23:22:56.451Z | 216.514° SW | 2026-04-14 23:25:56.451Z | 132.086° SE | 32.425° | 2026-04-14 23:28:56.451Z | 81.183° E |
| 6 mins | 2026-04-15 01:01:56.451Z | 270.409° WNW | 2026-04-15 01:03:56.451Z | 311.698° NW | 40.487° | 2026-04-15 01:07:56.451Z | 70.687° E |
| 6 mins | 2026-04-15 02:40:56.451Z | 292.55° NW | 2026-04-15 02:43:56.451Z | 36.599° NE | 37.687° | 2026-04-15 02:46:56.451Z | 84.612° E |
| 6 mins | 2026-04-15 04:19:56.451Z | 281.059° WNW | 2026-04-15 04:22:56.451Z | 162.737° S | 39.691° | 2026-04-15 04:25:56.451Z | 123.036° SE |
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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