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: 5 hours ago
TLE from 5 hours ago
0 YAM-15
1 68997U 26100T 26168.83335647 .00455079 00000-0 44575-1 0 9996
2 68997 97.7359 66.3002 0011097 91.9291 73.7166 14.90032099 5234Epoch: 2026-06-17T20:00Z
TLE epoch observation values (Epoch: 2026-06-17T20:00:01.999Z)
Latitude
14.0686°
Longitude
42.14674°
Altitude
597.975 km
Speed
7.563 km/s
True Right ascension
16h 32m 57s
True Declination
13° 59' 09"
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
12:10:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
602.594 km
Perigee altitude
587.118 km
Semi-major axis
6,972.993 km
Eccentricity
0.00111
Inclination
97.7359°
RAAN
66.3002°
Arg. of periapsis
91.9291°
True anomaly
73.83871°
Mean anomaly
73.7166°
Eccentric anomaly
73.77765°
Mean motion
3.72747 °/min
Orbital period
96.58 mins
BSTAR
0.044575
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-18 05:29:44.272Z | 31.199° NE | 2026-06-18 05:33:44.272Z | 106.2° ESE | 29.641° | 2026-06-18 05:36:44.272Z | 160.707° S |
| 5 mins | 2026-06-18 16:21:44.272Z | 110.715° ESE | 2026-06-18 16:23:44.272Z | 74.692° E | 21.394° | 2026-06-18 16:26:44.272Z | 21.252° NNE |
| 5 mins | 2026-06-18 17:57:44.272Z | 225.388° WSW | 2026-06-18 17:59:44.272Z | 270.02° WNW | 24.139° | 2026-06-18 18:02:44.272Z | 320.191° 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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