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 Commercial Imaging
Bus & Motor
ARROW, Unknown motor
Mass
~150 kg wet, ~140 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 2.3 m
Radar Cross Section
2.032 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 YAM-13
1 68993U 26100P 26266.02405939 .00000798 00000-0 87517-4 0 9994
2 68993 97.7759 161.8444 0001932 84.3733 275.7705 14.90419546 21270Epoch: 2026-09-23T00:34Z
TLE epoch observation values (Epoch: 2026-09-23T00:34:38.731Z)
Latitude
-0.00004°
Longitude
151.3019°
Altitude
599.531 km
Speed
7.56 km/s
True Right ascension
10h 47m 22s
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
05:22:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.995 km
Perigee altitude
592.301 km
Semi-major axis
6,971.785 km
Eccentricity
0.00019
Inclination
97.7759°
RAAN
161.8444°
Arg. of periapsis
84.3733°
True anomaly
275.74847°
Mean anomaly
275.7705°
Eccentric anomaly
275.75949°
Mean motion
3.72844 °/min
Orbital period
96.56 mins
BSTAR
0.000087517
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-23 16:48:35.888Z | 147.664° SSE | 2026-09-23 16:52:35.888Z | 67.214° ENE | 49.369° | 2026-09-23 16:55:35.888Z | 2.937° NNE |
| 6 mins | 2026-09-24 06:09:35.888Z | 7.234° NNE | 2026-09-24 06:12:35.888Z | 232.726° WSW | 70.312° | 2026-09-24 06:15:35.888Z | 199.318° 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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