Showing default

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.

Loading next visibility...
Identifier
68992, 2026-100N
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Airbus/Toulouse
Mission
Operational spacecraft
Bus & Motor
ARROW, Unknown motor
Mass
~150 kg wet, ~140 kg dry
Launch date (UTC)
2026-05-03 (2 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 YAM-16
1 68992U 26100N   26175.19580452  .00001448  00000-0  15029-3 0  9995
2 68992  97.7365  72.5000 0004748 109.6244 250.5487 14.91455102  7747
Epoch: 2026-06-24T04:41Z
TLE epoch observation values (Epoch: 2026-06-24T04:41:57.510Z)
Latitude
-0.00007°
Longitude
89.65389°
Altitude
597.543 km
Speed
7.56 km/s
True Right ascension
04h 50m 00s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
06:00:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
593.725 km
Perigee altitude
587.107 km
Semi-major axis
6,968.553 km
Eccentricity
0.00047
Inclination
97.7365°
RAAN
72.5°
Arg. of periapsis
109.6244°
True anomaly
250.49741°
Mean anomaly
250.5487°
Eccentric anomaly
250.52305°
Mean motion
3.73103 °/min
Orbital period
96.49 mins
BSTAR
0.00015029
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|