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 25310.30938655 .00000942 00000-0 11614-3 0 9997
2 40010 97.5541 156.4991 0008214 345.3689 14.7288 14.85075396615871Epoch: 2025-11-06T07:25Z
TLE epoch observation values (Epoch: 2025-11-06T07:25:30.997Z)
Latitude
-0.00002°
Longitude
-0.6496°
Altitude
610.833 km
Speed
7.557 km/s
True Right ascension
10h 25m 59s
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
13:36:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
616.108 km
Perigee altitude
604.628 km
Semi-major axis
6,988.505 km
Eccentricity
0.00082
Inclination
97.5541°
RAAN
156.4991°
Arg. of periapsis
345.3689°
True anomaly
14.75275°
Mean anomaly
14.7288°
Eccentric anomaly
14.74077°
Mean motion
3.71507 °/min
Orbital period
96.9 mins
BSTAR
0.00011614
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-07 01:48:18.876Z | 52.719° ENE | 2025-11-07 01:51:18.876Z | 103.181° ESE | 18.615° | 2025-11-07 01:53:18.876Z | 134.404° SE |
| 6 mins | 2025-11-07 03:24:18.876Z | 342.292° N | 2025-11-07 03:27:18.876Z | 275.995° WNW | 28.062° | 2025-11-07 03:30:18.876Z | 227.89° WSW |
| 6 mins | 2025-11-07 14:17:18.876Z | 196.114° SSW | 2025-11-07 14:19:18.876Z | 246.652° WSW | 36.9° | 2025-11-07 14:23:18.876Z | 335.074° NNW |
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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