OBJECT AF, 100912
Possibly "IRIDE-MS1-EAG2-17" | Orbit data source: Space-Track
OBJECT AF, 100912 is a payload satellite in SSO that was launched on Thu, 01 Oct 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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100912 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.368 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 OBJECT AF
1 A0912U 26227AF 26308.17518474 .00002656 00000-0 13468-3 0 9991
2 A0912 97.4425 17.1304 0003991 67.6259 292.5397 15.17802090 5070Epoch: 2026-11-04T04:12Z
TLE epoch observation values (Epoch: 2026-11-04T04:12:15.961Z)
Latitude
-0.00007°
Longitude
-89.36337°
Altitude
514.518 km
Speed
7.607 km/s
True Right ascension
01h 08m 31s
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
18:39:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.204 km
Perigee altitude
506.706 km
Semi-major axis
6,887.592 km
Eccentricity
0.0004
Inclination
97.4425°
RAAN
17.1304°
Arg. of periapsis
67.6259°
True anomaly
292.49745°
Mean anomaly
292.5397°
Eccentric anomaly
292.51858°
Mean motion
3.79701 °/min
Orbital period
94.81 mins
BSTAR
0.00013468
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Other satellites on launch #227 in the year 2026 (2026-10-01 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.OBJECT AF 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 | 2026-11-05 04:05:19.700Z | 116.043° SE | 2026-11-05 04:07:19.700Z | 73.863° E | 24.971° | 2026-11-05 04:10:19.700Z | 16.452° NNE |
| 5 mins | 2026-11-05 17:10:19.700Z | 36.482° NE | 2026-11-05 17:12:19.700Z | 78.877° E | 36.147° | 2026-11-05 17:15:19.700Z | 160.368° 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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