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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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: 22 hours ago
TLE from 22 hours ago
0 KAZEOSAT 2
1 40010U 14033A 26172.54108969 .00000113 00000-0 18924-4 0 9999
2 40010 97.5407 11.9225 0007483 313.6499 46.4096 14.85473699649606Epoch: 2026-06-21T12:59Z
TLE epoch observation values (Epoch: 2026-06-21T12:59:10.149Z)
Latitude
0.00001°
Longitude
-92.60967°
Altitude
611.534 km
Speed
7.555 km/s
True Right ascension
00h 47m 41s
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
21:42:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
614.346 km
Perigee altitude
603.889 km
Semi-major axis
6,987.254 km
Eccentricity
0.00075
Inclination
97.5407°
RAAN
11.9225°
Arg. of periapsis
313.6499°
True anomaly
46.47175°
Mean anomaly
46.4096°
Eccentric anomaly
46.44067°
Mean motion
3.71607 °/min
Orbital period
96.88 mins
BSTAR
0.000018924
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-22 13:21:11.295Z | 167.892° S | 2026-06-22 13:25:11.295Z | 331.371° NNW | 44.568° | 2026-06-22 13:29:11.295Z | 347.357° N |
| 6 mins | 2026-06-23 02:45:11.295Z | 340.12° N | 2026-06-23 02:47:11.295Z | 292.131° WNW | 31.283° | 2026-06-23 02:51:11.295Z | 221.076° 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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