STARLINK-30142, 56836
Orbit data source: Space-Track
STARLINK-30142, 56836 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 04 Jun 2023 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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56836 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 STARLINK-30142
1 56836U 23079P 26171.26373157 -.00001047 00000-0 -28531-4 0 9997
2 56836 43.0038 244.5278 0001318 253.3978 106.6729 15.27581016168619Epoch: 2026-06-20T06:19Z
TLE epoch observation values (Epoch: 2026-06-20T06:19:46.407Z)
Latitude
-0.00003°
Longitude
-118.89645°
Altitude
483.081 km
Speed
7.626 km/s
True Right ascension
16h 18m 06s
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
00:31:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.895 km
Perigee altitude
484.086 km
Semi-major axis
6,863.128 km
Eccentricity
0.00013
Inclination
43.0038°
RAAN
244.5278°
Arg. of periapsis
253.3978°
True anomaly
106.68737°
Mean anomaly
106.6729°
Eccentric anomaly
106.68013°
Mean motion
3.81733 °/min
Orbital period
94.31 mins
BSTAR
-0.000028531
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Other satellites on launch #79 in the year 2023 (2023-06-04 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-30142 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 | 2026-06-22 13:46:05.102Z | 260.787° W | 2026-06-22 13:48:05.102Z | 223.025° SW | 21.182° | 2026-06-22 13:51:05.102Z | 164.004° S |
| 5 mins | 2026-06-23 06:43:05.102Z | 190.189° SSW | 2026-06-23 06:45:05.102Z | 145.535° SSE | 23.024° | 2026-06-23 06:48:05.102Z | 90.793° ESE |
| 6 mins | 2026-06-23 08:21:05.102Z | 254.44° W | 2026-06-23 08:24:05.102Z | 55.293° ENE | 43.494° | 2026-06-23 08:27:05.102Z | 71.265° E |
| 5 mins | 2026-06-23 10:01:05.102Z | 295.597° NW | 2026-06-23 10:03:05.102Z | 12.901° NNE | 37.714° | 2026-06-23 10:06:05.102Z | 75.9° E |
| 5 mins | 2026-06-23 11:40:05.102Z | 289.232° WNW | 2026-06-23 11:42:05.102Z | 61.033° ENE | 44.948° | 2026-06-23 11:45:05.102Z | 107.712° ESE |
| 4 mins | 2026-06-23 13:19:05.102Z | 250.655° W | 2026-06-23 13:21:05.102Z | 203.999° SW | 21.589° | 2026-06-23 13:23:05.102Z | 166.259° S |
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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