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: 7 hours ago
TLE from 7 hours ago
0 YAM-5
1 55076U 23001BV 25336.12559905 .00013743 00000-0 42371-3 0 9992
2 55076 97.3512 34.8645 0011409 96.6622 263.5919 15.33650637161853Epoch: 2025-12-02T03:00Z
TLE epoch observation values (Epoch: 2025-12-02T03:00:51.757Z)
Latitude
-0.00011°
Longitude
-81.56637°
Altitude
468.922 km
Speed
7.631 km/s
True Right ascension
02h 19m 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
07:40:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.68 km
Perigee altitude
454.073 km
Semi-major axis
6,840.014 km
Eccentricity
0.00114
Inclination
97.3512°
RAAN
34.8645°
Arg. of periapsis
96.6622°
True anomaly
263.462°
Mean anomaly
263.5919°
Eccentric anomaly
263.52695°
Mean motion
3.8367 °/min
Orbital period
93.83 mins
BSTAR
0.00042371
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-02 16:07:29.379Z | 59.137° ENE | 2025-12-02 16:09:29.379Z | 100.372° ESE | 16.7° | 2025-12-02 16:11:29.379Z | 137.121° SSE |
| 5 mins | 2025-12-03 04:12:29.379Z | 173.557° S | 2025-12-03 04:14:29.379Z | 239.799° WSW | 44.346° | 2025-12-03 04:17:29.379Z | 344.839° N |
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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