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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Edit Public Description
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
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ALSAT 3A
1 67474U 26009A 26039.97578288 .00006882 00000-0 29114-3 0 9993
2 67474 97.4675 114.6335 0012459 168.9802 191.1710 15.23452837 3751Epoch: 2026-02-08T23:25Z
TLE epoch observation values (Epoch: 2026-02-08T23:25:07.640Z)
Latitude
-0.00006°
Longitude
-15.72556°
Altitude
506.932 km
Speed
7.606 km/s
True Right ascension
07h 38m 32s
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
10:20:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.959 km
Perigee altitude
483.839 km
Semi-major axis
6,870.536 km
Eccentricity
0.00125
Inclination
97.4675°
RAAN
114.6335°
Arg. of periapsis
168.9802°
True anomaly
191.14338°
Mean anomaly
191.171°
Eccentric anomaly
191.15719°
Mean motion
3.81116 °/min
Orbital period
94.46 mins
BSTAR
0.00029114
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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 | 2026-02-09 17:19:55.817Z | 34.528° NE | 2026-02-09 17:22:55.817Z | 119.909° SE | 30.793° | 2026-02-09 17:24:55.817Z | 162.356° S |
| 4 mins | 2026-02-10 05:30:55.817Z | 220.924° SW | 2026-02-10 05:32:55.817Z | 277.788° WNW | 25.717° | 2026-02-10 05:34:55.817Z | 318.361° NNW |
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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