STARLINK-35886, 66838
Orbit data source: Space-Track
STARLINK-35886, 66838 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 02 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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66838 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: 22 hours ago
TLE from 22 hours ago
0 STARLINK-35886
1 66838U 25280T 26170.93245649 .00001941 00000-0 17048-3 0 9994
2 66838 70.0014 76.5547 0002969 268.4564 91.6255 14.98324238 31398Epoch: 2026-06-19T22:22Z
TLE epoch observation values (Epoch: 2026-06-19T22:22:44.240Z)
Latitude
-0.00004°
Longitude
-167.28399°
Altitude
574.557 km
Speed
7.574 km/s
True Right ascension
05h 06m 13s
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
07:15:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.085 km
Perigee altitude
567.959 km
Semi-major axis
6,948.159 km
Eccentricity
0.0003
Inclination
70.0014°
RAAN
76.5547°
Arg. of periapsis
268.4564°
True anomaly
91.65951°
Mean anomaly
91.6255°
Eccentric anomaly
91.6425°
Mean motion
3.74747 °/min
Orbital period
96.06 mins
BSTAR
0.00017048
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Other satellites on launch #280 in the year 2025 (2025-12-02 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-35886 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 03:45:23.974Z | 7.453° NNE | 2026-06-21 03:48:23.974Z | 58.874° ENE | 21.075° | 2026-06-21 03:51:23.974Z | 107.354° ESE |
| 5 mins | 2026-06-21 05:24:23.974Z | 300.604° NW | 2026-06-21 05:26:23.974Z | 258.321° W | 26.711° | 2026-06-21 05:29:23.974Z | 198.097° SSW |
| 6 mins | 2026-06-21 19:24:23.974Z | 238.347° WSW | 2026-06-21 19:26:23.974Z | 289.298° WNW | 34.5° | 2026-06-21 19:30:23.974Z | 10.624° NNE |
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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