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 Defense Imaging
Bus & Motor
CAST-2000?, Unknown motor
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.8 m
Radar Cross Section
3.315 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ALSAT 3A
1 67474U 26009A 26171.47758172 .00005027 00000-0 21270-3 0 9992
2 67474 97.4541 245.3298 0014966 102.7088 257.5822 15.23553418 23772Epoch: 2026-06-20T11:27Z
TLE epoch observation values (Epoch: 2026-06-20T11:27:43.060Z)
Latitude
-0.00012°
Longitude
164.70876°
Altitude
500.454 km
Speed
7.613 km/s
True Right ascension
16h 21m 19s
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
07:18:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.378 km
Perigee altitude
481.814 km
Semi-major axis
6,870.233 km
Eccentricity
0.0015
Inclination
97.4541°
RAAN
245.3298°
Arg. of periapsis
102.7088°
True anomaly
257.41478°
Mean anomaly
257.5822°
Eccentric anomaly
257.49848°
Mean motion
3.81141 °/min
Orbital period
94.45 mins
BSTAR
0.0002127
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 04:55:52.938Z | 163.179° S | 2026-06-21 04:58:52.938Z | 21.953° NNE | 44.005° | 2026-06-21 05:01:52.938Z | 350.332° N |
| 5 mins | 2026-06-21 17:58:52.938Z | 2.659° NNE | 2026-06-21 18:00:52.938Z | 314.851° NW | 41.92° | 2026-06-21 18:03:52.938Z | 203.437° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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