STARLINK-36721, 67916
Orbit data source: Space-Track
STARLINK-36721, 67916 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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67916 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
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 STARLINK-36721
1 67916U 26036N 26071.85996092 -.00829466 00000-0 -47457-2 0 9996
2 67916 42.9982 230.2595 0002814 242.9338 117.1246 15.80036897 4178Epoch: 2026-03-12T20:38Z
TLE epoch observation values (Epoch: 2026-03-12T20:38:20.623Z)
Latitude
-0.00002°
Longitude
110.16976°
Altitude
330.967 km
Speed
7.711 km/s
True Right ascension
15h 21m 02s
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
12:21:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
334.214 km
Perigee altitude
330.437 km
Semi-major axis
6,710.463 km
Eccentricity
0.00028
Inclination
42.9982°
RAAN
230.2595°
Arg. of periapsis
242.9338°
True anomaly
117.15329°
Mean anomaly
117.1246°
Eccentric anomaly
117.13895°
Mean motion
3.94834 °/min
Orbital period
91.18 mins
BSTAR
-0.0047457
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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-36721 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 | 2026-03-13 13:32:29.496Z | 195.762° SSW | 2026-03-13 13:34:29.496Z | 139.781° SSE | 20.583° | 2026-03-13 13:36:29.496Z | 94.581° ESE |
| 4 mins | 2026-03-13 18:19:29.496Z | 287.824° WNW | 2026-03-13 18:21:29.496Z | 113.878° SE | 43.415° | 2026-03-13 18:23:29.496Z | 109.779° ESE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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