STARLINK-36265, 67208
Orbit data source: Space-Track
STARLINK-36265, 67208 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 17 Dec 2025 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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67208 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: 10 hours ago
TLE from 10 hours ago
0 STARLINK-36265
1 67208U 25304S 26171.44782554 .00002652 00000-0 22996-3 0 9999
2 67208 70.0008 275.4969 0003179 269.7303 90.3492 14.98337027 29273Epoch: 2026-06-20T10:44Z
TLE epoch observation values (Epoch: 2026-06-20T10:44:52.126Z)
Latitude
-0.00001°
Longitude
-154.38261°
Altitude
574.472 km
Speed
7.574 km/s
True Right ascension
18h 21m 59s
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
07:14:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.191 km
Perigee altitude
567.773 km
Semi-major axis
6,948.119 km
Eccentricity
0.00032
Inclination
70.0008°
RAAN
275.4969°
Arg. of periapsis
269.7303°
True anomaly
90.38563°
Mean anomaly
90.3492°
Eccentric anomaly
90.36741°
Mean motion
3.74751 °/min
Orbital period
96.06 mins
BSTAR
0.00022996
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Other satellites on launch #304 in the year 2025 (2025-12-17 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-36265 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 | 2026-06-21 07:42:23.645Z | 163.581° S | 2026-06-21 07:45:23.645Z | 105.74° ESE | 27.047° | 2026-06-21 07:48:23.645Z | 50.049° ENE |
| 5 mins | 2026-06-21 09:21:23.645Z | 262.406° W | 2026-06-21 09:23:23.645Z | 298.04° NW | 20.815° | 2026-06-21 09:26:23.645Z | 350.873° N |
| 6 mins | 2026-06-21 17:45:23.645Z | 346.543° N | 2026-06-21 17:47:23.645Z | 31.998° NE | 42.006° | 2026-06-21 17:51:23.645Z | 146.996° 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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