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: 7 hours ago
TLE from 7 hours ago
0 YAM-13
1 68993U 26100P 26317.71860998 .00001736 00000-0 18364-3 0 9993
2 68993 97.7733 212.7247 0001190 68.3844 291.7500 14.90458575 28970Epoch: 2026-11-13T17:14Z
TLE epoch observation values (Epoch: 2026-11-13T17:14:47.902Z)
Latitude
-0.00008°
Longitude
-98.80861°
Altitude
599.237 km
Speed
7.56 km/s
True Right ascension
14h 10m 53s
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
21:09:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.356 km
Perigee altitude
592.696 km
Semi-major axis
6,971.663 km
Eccentricity
0.00012
Inclination
97.7733°
RAAN
212.7247°
Arg. of periapsis
68.3844°
True anomaly
291.73733°
Mean anomaly
291.75°
Eccentric anomaly
291.74367°
Mean motion
3.72854 °/min
Orbital period
96.55 mins
BSTAR
0.00018364
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-14 05:07:17.430Z | 56.929° ENE | 2026-11-14 05:09:17.430Z | 91.167° ESE | 19.966° | 2026-11-14 05:12:17.430Z | 139.579° SSE |
| 5 mins | 2026-11-14 06:43:17.430Z | 332.648° NNW | 2026-11-14 06:45:17.430Z | 284.113° WNW | 31.517° | 2026-11-14 06:48:17.430Z | 230.615° WSW |
| 6 mins | 2026-11-14 17:33:17.430Z | 196.437° SSW | 2026-11-14 17:35:17.430Z | 250.923° W | 49.096° | 2026-11-14 17:39:17.430Z | 335.417° 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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