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 Technology
Bus & Motor
ARROW, Unknown motor
Mass
~150 kg wet, ~140 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 2.3 m
Radar Cross Section
0.035 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 YAM-14
1 69008U 26100AE 26201.73035913 .00000962 00000-0 10458-3 0 9992
2 69008 97.7842 98.4445 0005689 21.6057 338.5400 14.90362272 11680Epoch: 2026-07-20T17:31Z
TLE epoch observation values (Epoch: 2026-07-20T17:31:43.028Z)
Latitude
-0.00004°
Longitude
-102.99499°
Altitude
596.151 km
Speed
7.564 km/s
True Right ascension
06h 33m 46s
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
05:07:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
597.793 km
Perigee altitude
589.861 km
Semi-major axis
6,971.964 km
Eccentricity
0.00057
Inclination
97.7842°
RAAN
98.4445°
Arg. of periapsis
21.6057°
True anomaly
338.51613°
Mean anomaly
338.54°
Eccentric anomaly
338.52807°
Mean motion
3.7283 °/min
Orbital period
96.56 mins
BSTAR
0.00010458
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-07-21 16:13:55.893Z | 114.755° SE | 2026-07-21 16:16:55.893Z | 67.545° E | 19.205° | 2026-07-21 16:19:55.893Z | 20.467° NNE |
| 6 mins | 2026-07-21 17:49:55.893Z | 210.939° SW | 2026-07-21 17:51:55.893Z | 250.183° W | 26.883° | 2026-07-21 17:55:55.893Z | 325.378° NNW |
| 6 mins | 2026-07-22 05:33:55.893Z | 39.139° NE | 2026-07-22 05:35:55.893Z | 80.497° E | 31.426° | 2026-07-22 05:39:55.893Z | 165.804° 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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