STARLINK-36832, 68805
Orbit data source: Space-Track
STARLINK-36832, 68805 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Thu, 23 Apr 2026 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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68805 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, 14.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 STARLINK-36832
1 68805U 26089D 26170.56520193 .00009933 00000-0 30946-3 0 9998
2 68805 97.2852 17.5994 0001560 118.6172 241.5228 15.33458548 9015Epoch: 2026-06-19T13:33Z
TLE epoch observation values (Epoch: 2026-06-19T13:33:53.446Z)
Latitude
-0.00002°
Longitude
-93.66564°
Altitude
469.124 km
Speed
7.631 km/s
True Right ascension
01h 10m 23s
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
07:23:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.513 km
Perigee altitude
461.378 km
Semi-major axis
6,840.583 km
Eccentricity
0.00016
Inclination
97.2852°
RAAN
17.5994°
Arg. of periapsis
118.6172°
True anomaly
241.50709°
Mean anomaly
241.5228°
Eccentric anomaly
241.51494°
Mean motion
3.83622 °/min
Orbital period
93.84 mins
BSTAR
0.00030946
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Other satellites on launch #89 in the year 2026 (2026-04-23 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-36832 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 | 2026-06-21 02:08:59.726Z | 36.211° NE | 2026-06-21 02:11:59.726Z | 104.438° ESE | 26.44° | 2026-06-21 02:13:59.726Z | 151.752° SSE |
| 5 mins | 2026-06-21 14:14:59.726Z | 197.863° SSW | 2026-06-21 14:16:59.726Z | 255.898° W | 33.742° | 2026-06-21 14:19:59.726Z | 331.474° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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