YAM-13, 68993
Orbit data source: Space-Track
YAM-13, 68993 is an American payload satellite in SSO that was launched on Sun, 03 May 2026 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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68993 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Airbus/Toulouse
Mission
Operational spacecraft
Bus & Motor
ARROW, Unknown motor
Mass
~150 kg wet, ~140 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 YAM-13
1 68993U 26100P 26175.19005198 .00001340 00000-0 14320-3 0 9999
2 68993 97.7364 72.5070 0011117 62.6259 297.6089 14.90383206 7740Epoch: 2026-06-24T04:33Z
TLE epoch observation values (Epoch: 2026-06-24T04:33:40.491Z)
Latitude
0°
Longitude
91.73746°
Altitude
596.193 km
Speed
7.564 km/s
True Right ascension
04h 50m 01s
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
07:35:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
601.51 km
Perigee altitude
586.009 km
Semi-major axis
6,971.897 km
Eccentricity
0.00111
Inclination
97.7364°
RAAN
72.507°
Arg. of periapsis
62.6259°
True anomaly
297.49594°
Mean anomaly
297.6089°
Eccentric anomaly
297.55243°
Mean motion
3.72835 °/min
Orbital period
96.56 mins
BSTAR
0.0001432
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Other satellites on launch #100 in the year 2026 (2026-05-03 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-13 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 | 2026-06-25 05:18:19.265Z | 39.601° NE | 2026-06-25 05:21:19.265Z | 87.684° E | 23.588° | 2026-06-25 05:24:19.265Z | 145.701° SSE |
| 5 mins | 2026-06-25 06:55:19.265Z | 328.322° NNW | 2026-06-25 06:57:19.265Z | 288.059° WNW | 22.16° | 2026-06-25 07:00:19.265Z | 239.222° WSW |
| 6 mins | 2026-06-25 17:45:19.265Z | 205.649° SW | 2026-06-25 17:47:19.265Z | 246.899° WSW | 29.756° | 2026-06-25 17:51:19.265Z | 328.145° NNW |
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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