YAM-11, 68991
Orbit data source: Space-Track
YAM-11, 68991 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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68991 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: 9 hours ago
TLE from 9 hours ago
0 YAM-11
1 68991U 26100M 26266.13707170 .00001006 00000-0 10889-3 0 9996
2 68991 97.7723 161.8186 0001868 77.6017 282.5410 14.90420342 21286Epoch: 2026-09-23T03:17Z
TLE epoch observation values (Epoch: 2026-09-23T03:17:22.994Z)
Latitude
-0.00005°
Longitude
110.48028°
Altitude
599.381 km
Speed
7.56 km/s
True Right ascension
10h 47m 16s
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
05:23:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.948 km
Perigee altitude
592.343 km
Semi-major axis
6,971.782 km
Eccentricity
0.00019
Inclination
97.7723°
RAAN
161.8186°
Arg. of periapsis
77.6017°
True anomaly
282.5201°
Mean anomaly
282.541°
Eccentric anomaly
282.53055°
Mean motion
3.72844 °/min
Orbital period
96.56 mins
BSTAR
0.00010889
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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-11 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 | 2026-09-23 16:19:30.471Z | 117.156° SE | 2026-09-23 16:22:30.471Z | 65.223° ENE | 23.521° | 2026-09-23 16:25:30.471Z | 17.305° NNE |
| 5 mins | 2026-09-23 17:55:30.471Z | 216.838° SW | 2026-09-23 17:57:30.471Z | 254.618° W | 26.791° | 2026-09-23 18:00:30.471Z | 314.178° NW |
| 6 mins | 2026-09-24 05:39:30.471Z | 35.274° NE | 2026-09-24 05:41:30.471Z | 80.106° E | 44.582° | 2026-09-24 05:45:30.471Z | 171.394° S |
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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