STARLINK-4158, 53027
Orbit data source: Space-Track
STARLINK-4158, 53027 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 07 Jul 2022 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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53027 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK, Unknown motor
Mass
297 kg wet, ~275 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 10.1 m
Radar Cross Section
13.562 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 STARLINK-4158
1 53027U 22076AT 25343.82461137 .00001255 00000-0 96904-4 0 9998
2 53027 53.2179 127.5389 0001404 85.9506 274.1646 15.08842215189423Epoch: 2025-12-09T19:47Z
TLE epoch observation values (Epoch: 2025-12-09T19:47:26.422Z)
Latitude
-0.00007°
Longitude
111.87501°
Altitude
540.564 km
Speed
7.593 km/s
True Right ascension
08h 30m 09s
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
01:06:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.953 km
Perigee altitude
539.01 km
Semi-major axis
6,918.118 km
Eccentricity
0.00014
Inclination
53.2179°
RAAN
127.5389°
Arg. of periapsis
85.9506°
True anomaly
274.14855°
Mean anomaly
274.1646°
Eccentric anomaly
274.15658°
Mean motion
3.77191 °/min
Orbital period
95.44 mins
BSTAR
0.000096904
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Other satellites on launch #76 in the year 2022 (2022-07-07 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-4158 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 | 2025-12-10 11:50:16.577Z | 200.44° SSW | 2025-12-10 11:54:16.577Z | 116.328° SE | 31.183° | 2025-12-10 11:57:16.577Z | 65.908° ENE |
| 5 mins | 2025-12-10 13:31:16.577Z | 281.583° WNW | 2025-12-10 13:33:16.577Z | 331.914° NNW | 28.528° | 2025-12-10 13:36:16.577Z | 30.912° NE |
| 6 mins | 2025-12-10 18:32:16.577Z | 333.625° NNW | 2025-12-10 18:34:16.577Z | 21.896° NNE | 32.554° | 2025-12-10 18:38:16.577Z | 103.306° ESE |
| 5 mins | 2025-12-10 20:11:16.577Z | 280.826° WNW | 2025-12-10 20:13:16.577Z | 243.183° WSW | 25.34° | 2025-12-10 20:16:16.577Z | 177.579° S |
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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