STARLINK-30119, 56823
Orbit data source: Space-Track
STARLINK-30119, 56823 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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56823 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-30119
1 56823U 23079A 26171.20298619 .00000173 00000-0 15801-4 0 9999
2 56823 43.0003 248.3400 0001377 252.2489 107.8212 15.27580297168997Epoch: 2026-06-20T04:52Z
TLE epoch observation values (Epoch: 2026-06-20T04:52:18.006Z)
Latitude
-0.00006°
Longitude
-93.15607°
Altitude
483.113 km
Speed
7.626 km/s
True Right ascension
16h 33m 21s
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
00:39:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.938 km
Perigee altitude
484.048 km
Semi-major axis
6,863.13 km
Eccentricity
0.00014
Inclination
43.0003°
RAAN
248.34°
Arg. of periapsis
252.2489°
True anomaly
107.83622°
Mean anomaly
107.8212°
Eccentric anomaly
107.82871°
Mean motion
3.81733 °/min
Orbital period
94.31 mins
BSTAR
0.000015801
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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-30119 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 13:52:11.675Z | 265.368° W | 2026-06-22 13:55:11.675Z | 201.982° SSW | 23.133° | 2026-06-22 13:57:11.675Z | 163.137° S |
| 4 mins | 2026-06-23 06:50:11.675Z | 173.735° S | 2026-06-23 06:51:11.675Z | 150.979° SSE | 20.841° | 2026-06-23 06:54:11.675Z | 94.715° ESE |
| 5 mins | 2026-06-23 08:28:11.675Z | 250.743° W | 2026-06-23 08:30:11.675Z | 74.376° E | 44.765° | 2026-06-23 08:33:11.675Z | 71.945° E |
| 5 mins | 2026-06-23 10:07:11.675Z | 292° WNW | 2026-06-23 10:09:11.675Z | 359.37° N | 38.029° | 2026-06-23 10:12:11.675Z | 73.666° E |
| 5 mins | 2026-06-23 11:46:11.675Z | 290.719° WNW | 2026-06-23 11:48:11.675Z | 331.725° NNW | 44.407° | 2026-06-23 11:51:11.675Z | 104.134° ESE |
| 5 mins | 2026-06-23 13:25:11.675Z | 256.388° W | 2026-06-23 13:27:11.675Z | 209.105° SW | 23.996° | 2026-06-23 13:30:11.675Z | 154.991° SSE |
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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