YAM-14, 69008
Orbit data source: Space-Track
YAM-14, 69008 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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69008 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: 14 hours ago
TLE from 14 hours ago
0 YAM-14
1 69008U 26100AE 26220.72597381 .00000813 00000-0 89021-4 0 9992
2 69008 97.7815 117.1690 0002445 92.6855 267.4643 14.90471648 14514Epoch: 2026-08-08T17:25Z
TLE epoch observation values (Epoch: 2026-08-08T17:25:24.137Z)
Latitude
0.00001°
Longitude
-101.41476°
Altitude
599.579 km
Speed
7.56 km/s
True Right ascension
07h 48m 40s
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
21:25:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
595.19 km
Perigee altitude
591.781 km
Semi-major axis
6,971.622 km
Eccentricity
0.00024
Inclination
97.7815°
RAAN
117.169°
Arg. of periapsis
92.6855°
True anomaly
267.43631°
Mean anomaly
267.4643°
Eccentric anomaly
267.45031°
Mean motion
3.72857 °/min
Orbital period
96.55 mins
BSTAR
0.000089021
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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-14 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 | 2026-08-09 16:07:57.200Z | 107.789° ESE | 2026-08-09 16:10:57.200Z | 60.977° ENE | 16.775° | 2026-08-09 16:12:57.200Z | 29.813° NE |
| 5 mins | 2026-08-09 17:43:57.200Z | 209.835° SW | 2026-08-09 17:45:57.200Z | 260.208° W | 31.027° | 2026-08-09 17:48:57.200Z | 323.996° NNW |
| 5 mins | 2026-08-10 05:27:57.200Z | 48.901° ENE | 2026-08-10 05:29:57.200Z | 95.928° ESE | 28.53° | 2026-08-10 05:32:57.200Z | 156.089° SSE |
| 4 mins | 2026-08-10 07:03:57.200Z | 319.468° NNW | 2026-08-10 07:04:57.200Z | 301.652° NW | 18.231° | 2026-08-10 07:07:57.200Z | 251.197° W |
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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