KAZEOSAT 2, 40010
Orbit data source: Space-Track
KAZEOSAT 2, 40010 is a payload satellite owned by Kazkosmos (KZ) in SSO that was launched on Thu, 19 Jun 2014 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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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40010 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
KZ / KAZRelated business
Manufacturer
SSTL (Astrium)
Mission
Operational Civil Imaging
Bus & Motor
SSTL-150, AOCS
Mass
177 kg wet, 177 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.5 m
Radar Cross Section
1.500 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 KAZEOSAT 2
1 40010U 14033A 25340.29188328 .00001502 00000-0 18123-3 0 9997
2 40010 97.5516 184.9393 0007378 230.4969 129.5595 14.85152176620324Epoch: 2025-12-06T07:00Z
TLE epoch observation values (Epoch: 2025-12-06T07:00:18.715Z)
Latitude
-0.00002°
Longitude
4.5396°
Altitude
619.435 km
Speed
7.547 km/s
True Right ascension
12h 19m 45s
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
14:37:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
615.283 km
Perigee altitude
604.971 km
Semi-major axis
6,988.264 km
Eccentricity
0.00074
Inclination
97.5516°
RAAN
184.9393°
Arg. of periapsis
230.4969°
True anomaly
129.62464°
Mean anomaly
129.5595°
Eccentric anomaly
129.59208°
Mean motion
3.71526 °/min
Orbital period
96.9 mins
BSTAR
0.00018123
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Other satellites on launch #33 in the year 2014 (2014-06-19 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.KAZEOSAT 2 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 | 2025-12-07 02:59:44.892Z | 353.542° N | 2025-12-07 03:01:44.892Z | 299.514° NW | 39.354° | 2025-12-07 03:05:44.892Z | 209.102° SW |
| 7 mins | 2025-12-07 13:51:44.892Z | 168.243° S | 2025-12-07 13:54:44.892Z | 332.651° NNW | 44.579° | 2025-12-07 13:58:44.892Z | 347.393° N |
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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