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: 8 hours ago
TLE from 8 hours ago
0 KAZEOSAT 2
1 40010U 14033A 25286.59186581 .00000870 00000-0 10773-3 0 9998
2 40010 97.5580 133.9944 0009988 58.5758 301.6433 14.85022971612352Epoch: 2025-10-13T14:12Z
TLE epoch observation values (Epoch: 2025-10-13T14:12:17.205Z)
Latitude
-0.00006°
Longitude
-101.46972°
Altitude
612.893 km
Speed
7.555 km/s
True Right ascension
08h 55m 58s
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
17:00:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
617.513 km
Perigee altitude
603.553 km
Semi-major axis
6,988.67 km
Eccentricity
0.001
Inclination
97.558°
RAAN
133.9944°
Arg. of periapsis
58.5758°
True anomaly
301.5458°
Mean anomaly
301.6433°
Eccentric anomaly
301.59456°
Mean motion
3.71494 °/min
Orbital period
96.91 mins
BSTAR
0.00010773
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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 | 2025-10-14 02:06:06.750Z | 38.683° NE | 2025-10-14 02:09:06.750Z | 88.512° E | 25.431° | 2025-10-14 02:12:06.750Z | 147.898° SSE |
| 5 mins | 2025-10-14 03:43:06.750Z | 330.813° NNW | 2025-10-14 03:45:06.750Z | 294.632° NW | 21.364° | 2025-10-14 03:48:06.750Z | 243.852° WSW |
| 4 mins | 2025-10-14 13:01:06.750Z | 91.88° ESE | 2025-10-14 13:02:06.750Z | 73.586° E | 18.733° | 2025-10-14 13:05:06.750Z | 24.522° NE |
| 5 mins | 2025-10-14 14:36:06.750Z | 214.504° SW | 2025-10-14 14:38:06.750Z | 260.356° W | 28.55° | 2025-10-14 14:41:06.750Z | 321.042° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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