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: 7 hours ago
TLE from 7 hours ago
0 KAZEOSAT 2
1 40010U 14033A 26263.13767612 -.00000045 00000-0 63093-6 0 9995
2 40010 97.5364 97.7257 0009161 15.7370 344.4129 14.85561613663055Epoch: 2026-09-20T03:18Z
TLE epoch observation values (Epoch: 2026-09-20T03:18:15.216Z)
Latitude
-0.00004°
Longitude
49.12614°
Altitude
608.694 km
Speed
7.558 km/s
True Right ascension
06h 30m 54s
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
03:10:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
615.242 km
Perigee altitude
602.44 km
Semi-major axis
6,986.978 km
Eccentricity
0.00092
Inclination
97.5364°
RAAN
97.7257°
Arg. of periapsis
15.737°
True anomaly
344.38466°
Mean anomaly
344.4129°
Eccentric anomaly
344.39878°
Mean motion
3.71629 °/min
Orbital period
96.87 mins
BSTAR
6.3093e-7
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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 | 2026-09-20 13:06:46.863Z | 167.596° S | 2026-09-20 13:10:46.863Z | 182.356° SSW | 80.802° | 2026-09-20 13:14:46.863Z | 347.302° N |
| 4 mins | 2026-09-21 00:55:46.863Z | 68.85° E | 2026-09-21 00:56:46.863Z | 85.391° E | 17.435° | 2026-09-21 00:59:46.863Z | 132.109° SE |
| 6 mins | 2026-09-21 02:30:46.863Z | 344.709° N | 2026-09-21 02:33:46.863Z | 271.517° WNW | 36.307° | 2026-09-21 02:36:46.863Z | 223.338° SW |
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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