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: 15 hours ago
TLE from 15 hours ago
0 YAM-13
1 68993U 26100P 26220.70713344 .00000659 00000-0 73390-4 0 9991
2 68993 97.7828 117.2150 0001120 103.1199 257.0144 14.90390975 14525Epoch: 2026-08-08T16:58Z
TLE epoch observation values (Epoch: 2026-08-08T16:58:16.329Z)
Latitude
-0°
Longitude
-94.56765°
Altitude
599.93 km
Speed
7.56 km/s
True Right ascension
07h 48m 51s
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
22:28:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.518 km
Perigee altitude
592.956 km
Semi-major axis
6,971.874 km
Eccentricity
0.00011
Inclination
97.7828°
RAAN
117.215°
Arg. of periapsis
103.1199°
True anomaly
257.00189°
Mean anomaly
257.0144°
Eccentric anomaly
257.00815°
Mean motion
3.72837 °/min
Orbital period
96.56 mins
BSTAR
0.00007339
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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 | 2026-08-09 17:15:45.663Z | 171.295° S | 2026-08-09 17:18:45.663Z | 197.11° SSW | 42.982° | 2026-08-09 17:22:45.663Z | 344.449° N |
| 4 mins | 2026-08-10 05:01:45.663Z | 69.94° E | 2026-08-10 05:02:45.663Z | 86.624° E | 15.926° | 2026-08-10 05:05:45.663Z | 133.006° SE |
| 5 mins | 2026-08-10 06:36:45.663Z | 341.271° N | 2026-08-10 06:38:45.663Z | 292.902° NW | 31.162° | 2026-08-10 06:41:45.663Z | 227.408° WSW |
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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