STARLINK-36726, 67925
Orbit data source: Space-Track
STARLINK-36726, 67925 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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67925 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: 8 hours ago
TLE from 8 hours ago
0 STARLINK-36726
1 67925U 26036X 26104.20823219 .00006758 00000-0 25481-3 0 9995
2 67925 43.0012 44.7275 0001109 273.8668 86.2056 15.27587702 9157Epoch: 2026-04-14T04:59Z
TLE epoch observation values (Epoch: 2026-04-14T04:59:51.261Z)
Latitude
-0.00006°
Longitude
127.37606°
Altitude
482.751 km
Speed
7.626 km/s
True Right ascension
02h 58m 54s
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
19:21:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.732 km
Perigee altitude
484.21 km
Semi-major axis
6,863.108 km
Eccentricity
0.00011
Inclination
43.0012°
RAAN
44.7275°
Arg. of periapsis
273.8668°
True anomaly
86.21828°
Mean anomaly
86.2056°
Eccentric anomaly
86.21194°
Mean motion
3.81735 °/min
Orbital period
94.31 mins
BSTAR
0.00025481
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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-36726 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-14 22:26:16.536Z | 185.816° SSW | 2026-04-14 22:28:16.536Z | 152.98° SSE | 16.76° | 2026-04-14 22:31:16.536Z | 100.054° ESE |
| 5 mins | 2026-04-15 00:05:16.536Z | 241.008° WSW | 2026-04-15 00:07:16.536Z | 158.895° S | 44.205° | 2026-04-15 00:10:16.536Z | 74.243° E |
| 5 mins | 2026-04-15 01:44:16.536Z | 287.649° WNW | 2026-04-15 01:46:16.536Z | 350.46° N | 38.361° | 2026-04-15 01:49:16.536Z | 71.022° E |
| 6 mins | 2026-04-15 03:23:16.536Z | 292.874° NW | 2026-04-15 03:25:16.536Z | 336.45° NNW | 42.708° | 2026-04-15 03:29:16.536Z | 99.448° ESE |
| 5 mins | 2026-04-15 05:02:16.536Z | 263.408° W | 2026-04-15 05:04:16.536Z | 213.462° SW | 28.582° | 2026-04-15 05:07:16.536Z | 149.03° 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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