STARLINK-36898, 68002
Orbit data source: Space-Track
STARLINK-36898, 68002 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 27 Feb 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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68002 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: 2 days ago
TLE from 2 days ago
0 STARLINK-36898
1 68002U 26039S 26110.23419331 .00014268 00000-0 52692-3 0 9990
2 68002 42.9969 174.6069 0000415 68.8046 291.2850 15.27585067 8058Epoch: 2026-04-20T05:37Z
TLE epoch observation values (Epoch: 2026-04-20T05:37:14.301Z)
Latitude
-0.00003°
Longitude
-118.02998°
Altitude
482.706 km
Speed
7.626 km/s
True Right ascension
11h 38m 25s
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
18:10:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.264 km
Perigee altitude
484.695 km
Semi-major axis
6,863.117 km
Eccentricity
0.00004
Inclination
42.9969°
RAAN
174.6069°
Arg. of periapsis
68.8046°
True anomaly
291.28057°
Mean anomaly
291.285°
Eccentric anomaly
291.28278°
Mean motion
3.81734 °/min
Orbital period
94.31 mins
BSTAR
0.00052692
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Other satellites on launch #39 in the year 2026 (2026-02-27 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-36898 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-04-22 11:23:33.938Z | 288.506° WNW | 2026-04-22 11:26:33.938Z | 298.604° NW | 43.085° | 2026-04-22 11:30:33.938Z | 107.135° ESE |
| 4 mins | 2026-04-22 13:04:33.938Z | 240.651° WSW | 2026-04-22 13:05:33.938Z | 215.775° SW | 22.414° | 2026-04-22 13:08:33.938Z | 159.498° S |
| 4 mins | 2026-04-23 06:00:33.938Z | 183.216° SSW | 2026-04-23 06:02:33.938Z | 136.673° SSE | 21.6° | 2026-04-23 06:04:33.938Z | 98.655° ESE |
| 6 mins | 2026-04-23 07:38:33.938Z | 252.739° W | 2026-04-23 07:40:33.938Z | 261.213° W | 43.957° | 2026-04-23 07:44:33.938Z | 71.775° E |
| 6 mins | 2026-04-23 09:17:33.938Z | 288.657° WNW | 2026-04-23 09:19:33.938Z | 332.797° NNW | 36.606° | 2026-04-23 09:23:33.938Z | 76.857° E |
| 6 mins | 2026-04-23 10:56:33.938Z | 289.364° WNW | 2026-04-23 10:59:33.938Z | 93.241° ESE | 42.98° | 2026-04-23 11:02:33.938Z | 106.29° ESE |
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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