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 + 2 Pan, 17.7 m
Radar Cross Section
36.964 m²
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 STARLINK-36328
1 68096U 26042AD 26132.16668980 .00056382 00000-0 16695-2 0 9994
2 68096 53.1600 243.8814 0001639 95.2199 264.9747 15.34359478 5834Epoch: 2026-05-12T04:00Z
TLE epoch observation values (Epoch: 2026-05-12T04:00:01.998Z)
Latitude
0.06087°
Longitude
-46.02654°
Altitude
463.816 km
Speed
7.636 km/s
True Right ascension
16h 15m 42s
True Declination
0° 03' 38"
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
19:10:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.202 km
Perigee altitude
461.959 km
Semi-major axis
6,841.218 km
Eccentricity
0.00016
Inclination
53.16°
RAAN
243.8814°
Arg. of periapsis
95.2199°
True anomaly
264.95599°
Mean anomaly
264.9747°
Eccentric anomaly
264.96535°
Mean motion
3.83569 °/min
Orbital period
93.86 mins
BSTAR
0.0016695
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-12 12:05:02.411Z | 297.808° NW | 2026-05-12 12:07:02.411Z | 332.947° NNW | 16.285° | 2026-05-12 12:09:02.411Z | 11.98° NNE |
| 5 mins | 2026-05-12 17:01:02.411Z | 314.33° NW | 2026-05-12 17:03:02.411Z | 10.52° NNE | 44.386° | 2026-05-12 17:06:02.411Z | 126.249° SE |
| 5 mins | 2026-05-13 09:54:02.411Z | 219.847° SW | 2026-05-13 09:56:02.411Z | 79.906° E | 42.569° | 2026-05-13 09:59:02.411Z | 52.767° ENE |
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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