YAM-6, 59126
Orbit data source: Space-Track
YAM-6, 59126 is a payload satellite owned by Loft Orbital (US) in SSO that was launched on Mon, 04 Mar 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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59126 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-6
1 59126U 24043AE 25292.90212927 .00017315 00000-0 57037-3 0 9990
2 59126 97.5280 63.7750 0009438 12.7490 347.3988 15.31502625 90462Epoch: 2025-10-19T21:39Z
TLE epoch observation values (Epoch: 2025-10-19T21:39:03.968Z)
Latitude
-0.00004°
Longitude
70.39634°
Altitude
468.121 km
Speed
7.636 km/s
True Right ascension
04h 15m 06s
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
04:22:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
474.746 km
Perigee altitude
461.823 km
Semi-major axis
6,846.421 km
Eccentricity
0.00094
Inclination
97.528°
RAAN
63.775°
Arg. of periapsis
12.749°
True anomaly
347.37518°
Mean anomaly
347.3988°
Eccentric anomaly
347.38699°
Mean motion
3.83131 °/min
Orbital period
93.96 mins
BSTAR
0.00057037
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Other satellites on launch #43 in the year 2024 (2024-03-04 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.YAM-6 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 | 2025-10-20 21:43:35.114Z | 11.936° NNE | 2025-10-20 21:46:35.114Z | 9.636° NNE | 44.513° | 2025-10-20 21:49:35.114Z | 193.286° SSW |
| 4 mins | 2025-10-21 08:18:35.114Z | 108.425° ESE | 2025-10-21 08:19:35.114Z | 81.512° E | 24.485° | 2025-10-21 08:22:35.114Z | 14.467° 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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