YAM-5, 55076
Orbit data source: Space-Track
YAM-5, 55076 is a payload satellite owned by Loft Orbital (US) in SSO that was launched on Tue, 03 Jan 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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55076 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
LeoStella
Mission
Operational Commercial Technology
Bus & Motor
YAM, Unknown motor
Mass
87 kg wet, 87 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
1.500 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 YAM-5
1 55076U 23001BV 25286.90621466 .00014083 00000-0 45524-3 0 9995
2 55076 97.3575 345.9380 0008500 272.5092 87.5177 15.32159271154318Epoch: 2025-10-13T21:44Z
TLE epoch observation values (Epoch: 2025-10-13T21:44:56.946Z)
Latitude
-0.00001°
Longitude
-3.00155°
Altitude
472.232 km
Speed
7.63 km/s
True Right ascension
23h 03m 45s
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
02:52:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
472.137 km
Perigee altitude
460.501 km
Semi-major axis
6,844.456 km
Eccentricity
0.00085
Inclination
97.3575°
RAAN
345.938°
Arg. of periapsis
272.5092°
True anomaly
87.61502°
Mean anomaly
87.5177°
Eccentric anomaly
87.56636°
Mean motion
3.83296 °/min
Orbital period
93.92 mins
BSTAR
0.00045524
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Other satellites on launch #1 in the year 2023 (2023-01-03 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.YAM-5 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 | 2025-10-14 17:07:08.188Z | 2.114° NNE | 2025-10-14 17:10:08.188Z | 258.31° W | 40.281° | 2025-10-14 17:13:08.188Z | 204.453° SW |
| 4 mins | 2025-10-15 03:41:08.188Z | 123.074° SE | 2025-10-15 03:42:08.188Z | 94.746° ESE | 30.033° | 2025-10-15 03:45:08.188Z | 10.386° NNE |
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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