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 Defense 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 + 4 Pan, 0.1 m
Radar Cross Section
0.080 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-6
1 59126U 24043AE 25259.63466131 .00010304 00000-0 35114-3 0 9994
2 59126 97.5227 30.0312 0010665 121.4303 238.7982 15.30519188 85371Epoch: 2025-09-16T15:13Z
TLE epoch observation values (Epoch: 2025-09-16T15:13:54.737Z)
Latitude
0.00003°
Longitude
165.73098°
Altitude
481.156 km
Speed
7.623 km/s
True Right ascension
02h 00m 07s
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
14:47:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
478.524 km
Perigee altitude
463.914 km
Semi-major axis
6,849.356 km
Eccentricity
0.00107
Inclination
97.5227°
RAAN
30.0312°
Arg. of periapsis
121.4303°
True anomaly
238.69374°
Mean anomaly
238.7982°
Eccentric anomaly
238.74596°
Mean motion
3.82885 °/min
Orbital period
94.02 mins
BSTAR
0.00035114
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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 | 2025-09-16 22:03:25.240Z | 356.425° N | 2025-09-16 22:06:25.240Z | 297.616° NW | 32.255° | 2025-09-16 22:09:25.240Z | 219.379° SW |
| 5 mins | 2025-09-17 08:38:25.240Z | 146.996° SSE | 2025-09-17 08:40:25.240Z | 52.58° ENE | 40.32° | 2025-09-17 08:43:25.240Z | 356.018° N |
| 5 mins | 2025-09-17 21:37:25.240Z | 17.482° NNE | 2025-09-17 21:39:25.240Z | 157.354° SSE | 43.725° | 2025-09-17 21:42:25.240Z | 189.484° SSW |
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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