STARLINK-36328, 68096
Orbit data source: Space-Track
STARLINK-36328, 68096 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 04 Mar 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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68096 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 + 1 Pan, 17.7 m
Radar Cross Section
41.120 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 STARLINK-36328
1 68096U 26042AD 26228.17717740 .00023456 00000-0 70340-3 0 9994
2 68096 53.1584 155.0618 0001256 82.3879 277.7266 15.34390326 26757Epoch: 2026-08-16T04:15Z
TLE epoch observation values (Epoch: 2026-08-16T04:15:08.127Z)
Latitude
-0.00003°
Longitude
126.70047°
Altitude
463.518 km
Speed
7.636 km/s
True Right ascension
10h 20m 14s
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
11:21:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.848 km
Perigee altitude
462.13 km
Semi-major axis
6,841.126 km
Eccentricity
0.00013
Inclination
53.1584°
RAAN
155.0618°
Arg. of periapsis
82.3879°
True anomaly
277.71234°
Mean anomaly
277.7266°
Eccentric anomaly
277.71947°
Mean motion
3.83576 °/min
Orbital period
93.85 mins
BSTAR
0.0007034
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Other satellites on launch #42 in the year 2026 (2026-03-04 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-36328 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 | 2026-08-16 21:37:06.260Z | 211.982° SW | 2026-08-16 21:40:06.260Z | 123.46° SE | 39.362° | 2026-08-16 21:43:06.260Z | 58.919° ENE |
| 4 mins | 2026-08-16 23:16:06.260Z | 295.256° NW | 2026-08-16 23:18:06.260Z | 341.798° N | 20.811° | 2026-08-16 23:20:06.260Z | 21.056° NNE |
| 5 mins | 2026-08-17 04:12:06.260Z | 334.007° NNW | 2026-08-17 04:14:06.260Z | 52.176° ENE | 35.505° | 2026-08-17 04:17:06.260Z | 109.749° ESE |
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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