YAM-16, 68992
Orbit data source: Space-Track
YAM-16, 68992 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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68992 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: 10 hours ago
TLE from 10 hours ago
0 YAM-16
1 68992U 26100N 26220.94923091 .00000705 00000-0 75803-4 0 9991
2 68992 97.7299 117.3689 0002989 357.9992 2.1214 14.91577826 14562Epoch: 2026-08-08T22:46Z
TLE epoch observation values (Epoch: 2026-08-08T22:46:53.550Z)
Latitude
-0.00006°
Longitude
178.19254°
Altitude
593.975 km
Speed
7.564 km/s
True Right ascension
07h 49m 28s
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
592.116 km
Perigee altitude
587.95 km
Semi-major axis
6,968.17 km
Eccentricity
0.0003
Inclination
97.7299°
RAAN
117.3689°
Arg. of periapsis
357.9992°
True anomaly
2.12267°
Mean anomaly
2.1214°
Eccentric anomaly
2.12203°
Mean motion
3.73134 °/min
Orbital period
96.48 mins
BSTAR
0.000075803
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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-16 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 | 2026-08-09 16:37:45.130Z | 132.874° SE | 2026-08-09 16:40:45.130Z | 72.076° E | 30.474° | 2026-08-09 16:43:45.130Z | 10.71° NNE |
| 4 mins | 2026-08-09 18:14:45.130Z | 238.256° WSW | 2026-08-09 18:16:45.130Z | 272.331° WNW | 16.279° | 2026-08-09 18:18:45.130Z | 303.425° NW |
| 7 mins | 2026-08-10 05:56:45.130Z | 17.248° NNE | 2026-08-10 05:59:45.130Z | 88.311° E | 44.123° | 2026-08-10 06:03:45.130Z | 188.018° 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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