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: 12 hours ago
TLE from 12 hours ago
0 YAM-5
1 55076U 23001BV 26023.62315778 .00016347 00000-0 48114-3 0 9993
2 55076 97.3413 87.1162 0007993 267.3316 92.7013 15.35113181169909Epoch: 2026-01-23T14:57Z
TLE epoch observation values (Epoch: 2026-01-23T14:57:20.832Z)
Latitude
0.00003°
Longitude
99.82008°
Altitude
463.959 km
Speed
7.634 km/s
True Right ascension
05h 48m 27s
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
04:13:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
462.991 km
Perigee altitude
452.064 km
Semi-major axis
6,835.664 km
Eccentricity
0.0008
Inclination
97.3413°
RAAN
87.1162°
Arg. of periapsis
267.3316°
True anomaly
92.79279°
Mean anomaly
92.7013°
Eccentric anomaly
92.74704°
Mean motion
3.84036 °/min
Orbital period
93.74 mins
BSTAR
0.00048114
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-01-24 03:37:09.166Z | 123.818° SE | 2026-01-24 03:39:09.166Z | 73.255° E | 26.402° | 2026-01-24 03:42:09.166Z | 10.775° NNE |
| 4 mins | 2026-01-24 16:34:09.166Z | 45.169° ENE | 2026-01-24 16:36:09.166Z | 112.186° ESE | 30.293° | 2026-01-24 16:38:09.166Z | 159.882° 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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