AIGLONSAT-1, 68437
Orbit data source: Space-Track
AIGLONSAT-1, 68437 is an American payload satellite in SSO that was launched on Mon, 30 Mar 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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68437 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
AIGLON
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1.7 kg wet, 1.7 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 AIGLONSAT-1
1 68437U 26067X 26262.33355171 .00011505 00000-0 50670-3 0 9998
2 68437 97.4600 219.8206 0004923 82.9640 277.2156 15.21980786 26253Epoch: 2026-09-19T08:00Z
TLE epoch observation values (Epoch: 2026-09-19T08:00:18.867Z)
Latitude
-0.00002°
Longitude
101.4984°
Altitude
502.534 km
Speed
7.613 km/s
True Right ascension
14h 39m 16s
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
05:12:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.217 km
Perigee altitude
493.447 km
Semi-major axis
6,874.969 km
Eccentricity
0.00049
Inclination
97.46°
RAAN
219.8206°
Arg. of periapsis
82.964°
True anomaly
277.15963°
Mean anomaly
277.2156°
Eccentric anomaly
277.18761°
Mean motion
3.80747 °/min
Orbital period
94.55 mins
BSTAR
0.0005067
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Other satellites on launch #67 in the year 2026 (2026-03-30 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.AIGLONSAT-1 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-20 20:27:15.530Z | 104.891° ESE | 2026-09-20 20:29:15.530Z | 65.406° ENE | 18.899° | 2026-09-20 20:31:15.530Z | 28.56° NE |
| 4 mins | 2026-09-20 22:01:15.530Z | 228.803° WSW | 2026-09-20 22:02:15.530Z | 252.341° W | 24.595° | 2026-09-20 22:05:15.530Z | 316.383° NNW |
| 5 mins | 2026-09-21 09:30:15.530Z | 51.524° ENE | 2026-09-21 09:32:15.530Z | 98.377° ESE | 26.066° | 2026-09-21 09:35:15.530Z | 154.393° SSE |
| 4 mins | 2026-09-21 11:04:15.530Z | 321.004° NNW | 2026-09-21 11:05:15.530Z | 301.788° NW | 17.996° | 2026-09-21 11:08:15.530Z | 247.133° WSW |
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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