YAM-7, 60504
Orbit data source: Space-Track
YAM-7, 60504 is an American payload satellite in SSO that was launched on Fri, 16 Aug 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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60504 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
LeoStella
Mission
Operational Commercial Technology
Bus & Motor
YAM, Unknown motor
Mass
91 kg wet, 91 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.875 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-7
1 60504U 24149AN 26252.75349849 .00005768 00000-0 18432-3 0 9998
2 60504 97.3738 332.6952 0003424 20.6579 339.4801 15.32840756115002Epoch: 2026-09-09T18:05Z
TLE epoch observation values (Epoch: 2026-09-09T18:05:02.269Z)
Latitude
-0.00002°
Longitude
72.63472°
Altitude
468.255 km
Speed
7.633 km/s
True Right ascension
22h 10m 46s
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
14:58:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.632 km
Perigee altitude
461.946 km
Semi-major axis
6,842.426 km
Eccentricity
0.00034
Inclination
97.3738°
RAAN
332.6952°
Arg. of periapsis
20.6579°
True anomaly
339.46634°
Mean anomaly
339.4801°
Eccentric anomaly
339.47322°
Mean motion
3.83467 °/min
Orbital period
93.88 mins
BSTAR
0.00018432
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Other satellites on launch #149 in the year 2024 (2024-08-16 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-7 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 | 2026-09-11 04:42:15.200Z | 111.161° ESE | 2026-09-11 04:44:15.200Z | 69.551° E | 20.438° | 2026-09-11 04:46:15.200Z | 28.289° NE |
| 4 mins | 2026-09-11 17:40:15.200Z | 55.267° ENE | 2026-09-11 17:42:15.200Z | 106.474° ESE | 24.72° | 2026-09-11 17:44:15.200Z | 147.45° SSE |
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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