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 26217.41226635 .00009217 00000-0 41959-3 0 9996
2 68437 97.4533 175.3208 0001811 154.9297 205.2027 15.20915456 19427Epoch: 2026-08-05T09:53Z
TLE epoch observation values (Epoch: 2026-08-05T09:53:39.812Z)
Latitude
-0.00001°
Longitude
72.93788°
Altitude
507.296 km
Speed
7.61 km/s
True Right ascension
11h 41m 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
00:07:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.29 km
Perigee altitude
498.799 km
Semi-major axis
6,878.182 km
Eccentricity
0.00018
Inclination
97.4533°
RAAN
175.3208°
Arg. of periapsis
154.9297°
True anomaly
205.19386°
Mean anomaly
205.2027°
Eccentric anomaly
205.19828°
Mean motion
3.80481 °/min
Orbital period
94.62 mins
BSTAR
0.00041959
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-06 10:08:25.784Z | 11.647° NNE | 2026-08-06 10:11:25.784Z | 345.498° N | 44.964° | 2026-08-06 10:14:25.784Z | 193.544° SSW |
| 4 mins | 2026-08-06 20:47:25.784Z | 116.334° SE | 2026-08-06 20:49:25.784Z | 54.656° ENE | 27.663° | 2026-08-06 20:51:25.784Z | 14.335° NNE |
| 5 mins | 2026-08-07 09:50:25.784Z | 30.523° NE | 2026-08-07 09:52:25.784Z | 80.693° E | 36.625° | 2026-08-07 09:55:25.784Z | 171.671° 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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