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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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: 1 day ago
TLE from 1 day ago
0 YAM-6
1 59126U 24043AE 26191.35421513 .00006722 00000-0 18458-3 0 9995
2 59126 97.5583 333.1400 0009267 140.1427 220.0499 15.37548735130872Epoch: 2026-07-10T08:30Z
TLE epoch observation values (Epoch: 2026-07-10T08:30:04.187Z)
Latitude
-0.00005°
Longitude
-82.66043°
Altitude
461.32 km
Speed
7.633 km/s
True Right ascension
22h 12m 33s
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
02:33:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
456.638 km
Perigee altitude
443.982 km
Semi-major axis
6,828.447 km
Eccentricity
0.00093
Inclination
97.5583°
RAAN
333.14°
Arg. of periapsis
140.1427°
True anomaly
219.98163°
Mean anomaly
220.0499°
Eccentric anomaly
220.01576°
Mean motion
3.84645 °/min
Orbital period
93.59 mins
BSTAR
0.00018458
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-07-11 22:32:53.558Z | 3.264° NNE | 2026-07-11 22:35:53.558Z | 240.247° WSW | 39.378° | 2026-07-11 22:37:53.558Z | 205.445° SW |
| 4 mins | 2026-07-12 09:04:53.558Z | 113.558° SE | 2026-07-12 09:05:53.558Z | 80.912° E | 28.685° | 2026-07-12 09:08:53.558Z | 9.195° 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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