STARLINK-36532, 67628
Orbit data source: Space-Track
STARLINK-36532, 67628 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 30 Jan 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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67628 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: 11 hours ago
TLE from 11 hours ago
0 STARLINK-36532
1 67628U 26020M 26104.57390487 .00010963 00000-0 40724-3 0 9994
2 67628 43.0019 296.9392 0001189 279.1033 80.9685 15.27585049 11602Epoch: 2026-04-14T13:46Z
TLE epoch observation values (Epoch: 2026-04-14T13:46:25.380Z)
Latitude
0.00003°
Longitude
-112.41472°
Altitude
482.682 km
Speed
7.626 km/s
True Right ascension
19h 47m 45s
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
07:04:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.795 km
Perigee altitude
484.163 km
Semi-major axis
6,863.116 km
Eccentricity
0.00012
Inclination
43.0019°
RAAN
296.9392°
Arg. of periapsis
279.1033°
True anomaly
80.98196°
Mean anomaly
80.9685°
Eccentric anomaly
80.97523°
Mean motion
3.81734 °/min
Orbital period
94.31 mins
BSTAR
0.00040724
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Other satellites on launch #20 in the year 2026 (2026-01-30 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-36532 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 | 2026-04-15 15:03:30.912Z | 185.666° SSW | 2026-04-15 15:05:30.912Z | 153.501° SSE | 16.356° | 2026-04-15 15:08:30.912Z | 100.783° ESE |
| 5 mins | 2026-04-15 16:42:30.912Z | 240.158° WSW | 2026-04-15 16:44:30.912Z | 165.078° S | 44.029° | 2026-04-15 16:47:30.912Z | 74.551° E |
| 5 mins | 2026-04-15 18:21:30.912Z | 287.022° WNW | 2026-04-15 18:23:30.912Z | 348.357° N | 38.381° | 2026-04-15 18:26:30.912Z | 70.699° E |
| 6 mins | 2026-04-15 20:00:30.912Z | 292.943° NW | 2026-04-15 20:02:30.912Z | 334.898° NNW | 42.405° | 2026-04-15 20:06:30.912Z | 98.875° ESE |
| 5 mins | 2026-04-15 21:39:30.912Z | 264.304° W | 2026-04-15 21:41:30.912Z | 214.633° SW | 29.019° | 2026-04-15 21:44:30.912Z | 148.542° 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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