STARLINK-36489, 67328
Orbit data source: Space-Track
STARLINK-36489, 67328 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 04 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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67328 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
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 STARLINK-36489
1 67328U 26002Z 26063.83048214 .00044110 00000-0 16017-2 0 9990
2 67328 43.0010 352.8861 0001907 262.4561 97.6074 15.27603258 10498Epoch: 2026-03-04T19:55Z
TLE epoch observation values (Epoch: 2026-03-04T19:55:53.656Z)
Latitude
-0.00004°
Longitude
-108.67707°
Altitude
482.928 km
Speed
7.626 km/s
True Right ascension
23h 31m 32s
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
04:30:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.233 km
Perigee altitude
483.616 km
Semi-major axis
6,863.061 km
Eccentricity
0.00019
Inclination
43.001°
RAAN
352.8861°
Arg. of periapsis
262.4561°
True anomaly
97.62906°
Mean anomaly
97.6074°
Eccentric anomaly
97.61823°
Mean motion
3.81739 °/min
Orbital period
94.31 mins
BSTAR
0.0016017
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Other satellites on launch #2 in the year 2026 (2026-01-04 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-36489 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 | 2026-03-05 00:57:09.112Z | 277.581° WNW | 2026-03-05 01:00:09.112Z | 359.585° N | 39.246° | 2026-03-05 01:03:09.112Z | 70.295° E |
| 5 mins | 2026-03-05 02:37:09.112Z | 295.271° NW | 2026-03-05 02:39:09.112Z | 357.64° N | 41.776° | 2026-03-05 02:42:09.112Z | 91.601° ESE |
| 5 mins | 2026-03-05 04:16:09.112Z | 267.471° W | 2026-03-05 04:18:09.112Z | 208.951° SW | 33.541° | 2026-03-05 04:21:09.112Z | 140.278° SSE |
| 5 mins | 2026-03-05 22:51:09.112Z | 229.811° WSW | 2026-03-05 22:53:09.112Z | 163.944° S | 41.226° | 2026-03-05 22:56:09.112Z | 77.856° E |
| 5 mins | 2026-03-06 00:30:09.112Z | 282.613° WNW | 2026-03-06 00:32:09.112Z | 346.276° N | 39.355° | 2026-03-06 00:35:09.112Z | 69.33° E |
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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