STARLINK-36700, 67662
Orbit data source: Space-Track
STARLINK-36700, 67662 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Mon, 02 Feb 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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67662 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: 13 hours ago
TLE from 13 hours ago
0 STARLINK-36700
1 67662U 26022Q 26095.08808834 .00032305 00000-0 99935-3 0 9991
2 67662 97.2841 129.1325 0001780 101.1577 258.9866 15.33423399 9624Epoch: 2026-04-05T02:06Z
TLE epoch observation values (Epoch: 2026-04-05T02:06:50.832Z)
Latitude
-0.00002°
Longitude
-95.97783°
Altitude
468.952 km
Speed
7.632 km/s
True Right ascension
08h 36m 31s
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
20:58:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.768 km
Perigee altitude
461.333 km
Semi-major axis
6,840.687 km
Eccentricity
0.00018
Inclination
97.2841°
RAAN
129.1325°
Arg. of periapsis
101.1577°
True anomaly
258.96658°
Mean anomaly
258.9866°
Eccentric anomaly
258.97659°
Mean motion
3.83613 °/min
Orbital period
93.84 mins
BSTAR
0.00099935
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Other satellites on launch #22 in the year 2026 (2026-02-02 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-36700 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 | 2026-04-05 15:11:41.521Z | 6.913° NNE | 2026-04-05 15:14:41.521Z | 318.102° NNW | 42.709° | 2026-04-05 15:17:41.521Z | 200.835° SSW |
| 4 mins | 2026-04-06 01:45:41.521Z | 117.812° SE | 2026-04-06 01:47:41.521Z | 56.12° ENE | 26.532° | 2026-04-06 01:49:41.521Z | 14.675° NNE |
| 5 mins | 2026-04-06 14:42:41.521Z | 38.036° NE | 2026-04-06 14:44:41.521Z | 99.013° ESE | 32.832° | 2026-04-06 14:47:41.521Z | 168.528° S |
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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