YAM-15, 68997
Orbit data source: Space-Track
YAM-15, 68997 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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68997 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Airbus/Toulouse
Mission
Operational spacecraft
Bus & Motor
ARROW, Unknown motor
Mass
~150 kg wet, ~140 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 YAM-15
1 68997U 26100T 26175.17987260 .00001258 00000-0 13405-3 0 9991
2 68997 97.7358 72.5161 0010711 74.0396 286.2001 14.90594324 7749Epoch: 2026-06-24T04:19Z
TLE epoch observation values (Epoch: 2026-06-24T04:19:00.992Z)
Latitude
-0.00008°
Longitude
95.42119°
Altitude
597.045 km
Speed
7.562 km/s
True Right ascension
04h 50m 03s
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
09:08:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
600.568 km
Perigee altitude
585.634 km
Semi-major axis
6,971.238 km
Eccentricity
0.00107
Inclination
97.7358°
RAAN
72.5161°
Arg. of periapsis
74.0396°
True anomaly
286.08219°
Mean anomaly
286.2001°
Eccentric anomaly
286.14115°
Mean motion
3.72888 °/min
Orbital period
96.54 mins
BSTAR
0.00013405
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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-15 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 | 2026-06-25 05:04:31.984Z | 55.875° ENE | 2026-06-25 05:06:31.984Z | 87.617° E | 17.095° | 2026-06-25 05:09:31.984Z | 135.447° SSE |
| 5 mins | 2026-06-25 06:40:31.984Z | 337.892° N | 2026-06-25 06:42:31.984Z | 289.793° WNW | 29.391° | 2026-06-25 06:45:31.984Z | 229.285° WSW |
| 6 mins | 2026-06-25 17:30:31.984Z | 189.945° SSW | 2026-06-25 17:32:31.984Z | 236.359° WSW | 38.288° | 2026-06-25 17:36:31.984Z | 336.73° NNW |
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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