STARLINK-37146, 68555
Orbit data source: Space-Track
STARLINK-37146, 68555 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 02 Apr 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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68555 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: 1 day ago
TLE from 1 day ago
0 STARLINK-37146
1 68555U 26070P 26246.40869535 .00016475 00000-0 49771-3 0 9998
2 68555 53.1588 253.5929 0001345 81.1183 278.9972 15.34397163 23811Epoch: 2026-09-03T09:48Z
TLE epoch observation values (Epoch: 2026-09-03T09:48:31.278Z)
Latitude
0.00001°
Longitude
123.91529°
Altitude
463.469 km
Speed
7.636 km/s
True Right ascension
16h 54m 22s
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
01:37:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.889 km
Perigee altitude
462.049 km
Semi-major axis
6,841.106 km
Eccentricity
0.00013
Inclination
53.1588°
RAAN
253.5929°
Arg. of periapsis
81.1183°
True anomaly
278.98198°
Mean anomaly
278.9972°
Eccentric anomaly
278.98959°
Mean motion
3.83578 °/min
Orbital period
93.85 mins
BSTAR
0.00049771
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Other satellites on launch #70 in the year 2026 (2026-04-02 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-37146 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 | 2026-09-04 09:45:03.106Z | 319.813° NNW | 2026-09-04 09:48:03.106Z | 69.286° E | 39.315° | 2026-09-04 09:51:03.106Z | 117.641° SE |
| 5 mins | 2026-09-05 02:38:03.106Z | 208.217° SW | 2026-09-05 02:40:03.106Z | 150.445° SSE | 39.369° | 2026-09-05 02:43:03.106Z | 60.222° ENE |
| 5 mins | 2026-09-05 09:12:03.106Z | 329.765° NNW | 2026-09-05 09:14:03.106Z | 33.02° NE | 36.166° | 2026-09-05 09:17:03.106Z | 108.095° 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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