ALSAT 3A, 67474
Orbit data source: Space-Track
ALSAT 3A, 67474 is a payload satellite owned by ASAL (DZ) in SSO that was launched on Thu, 15 Jan 2026 UTC via a CHANG ZHENG 2C launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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67474 intel report (Beta)
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Identifier
Orbit
Country
DZ / ALGRelated business
Manufacturer
CAST
Mission
Operational spacecraft
Bus & Motor
CAST-2000?, Unknown motor
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 ALSAT 3A
1 67474U 26009A 26065.78574468 .00008480 00000-0 35366-3 0 9999
2 67474 97.4624 140.3172 0013541 86.4267 273.8519 15.23850985 7689Epoch: 2026-03-06T18:51Z
TLE epoch observation values (Epoch: 2026-03-06T18:51:28.340Z)
Latitude
0.00004°
Longitude
52.93235°
Altitude
496.719 km
Speed
7.617 km/s
True Right ascension
09h 21m 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
08:35:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.503 km
Perigee altitude
481.899 km
Semi-major axis
6,869.338 km
Eccentricity
0.00135
Inclination
97.4624°
RAAN
140.3172°
Arg. of periapsis
86.4267°
True anomaly
273.69706°
Mean anomaly
273.8519°
Eccentric anomaly
273.77448°
Mean motion
3.81216 °/min
Orbital period
94.43 mins
BSTAR
0.00035366
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Other satellites on launch #9 in the year 2026 (2026-01-15 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.ALSAT 3A 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 | 2026-03-07 17:29:52.903Z | 30.612° NE | 2026-03-07 17:31:52.903Z | 90.339° ESE | 37.87° | 2026-03-07 17:34:52.903Z | 174.342° S |
| 4 mins | 2026-03-08 04:06:52.903Z | 102.147° ESE | 2026-03-08 04:08:52.903Z | 58.935° ENE | 18.171° | 2026-03-08 04:10:52.903Z | 23.934° NE |
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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