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: 15 hours ago
TLE from 15 hours ago
0 KAZEOSAT 2
1 40010U 14033A 25256.26980465 .00000482 00000-0 62456-4 0 9997
2 40010 97.5638 105.2104 0009440 145.0464 215.1373 14.84949780607851Epoch: 2025-09-13T06:28Z
TLE epoch observation values (Epoch: 2025-09-13T06:28:31.121Z)
Latitude
-0.00005°
Longitude
15.57516°
Altitude
622.182 km
Speed
7.545 km/s
True Right ascension
07h 00m 50s
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
14:26:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
617.36 km
Perigee altitude
604.165 km
Semi-major axis
6,988.9 km
Eccentricity
0.00094
Inclination
97.5638°
RAAN
105.2104°
Arg. of periapsis
145.0464°
True anomaly
215.0751°
Mean anomaly
215.1373°
Eccentric anomaly
215.10619°
Mean motion
3.71475 °/min
Orbital period
96.91 mins
BSTAR
0.000062456
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-14 02:26:51.424Z | 26.248° NE | 2025-09-14 02:30:51.424Z | 103.046° ESE | 34.835° | 2025-09-14 02:33:51.424Z | 166.474° S |
| 5 mins | 2025-09-14 13:21:51.424Z | 110.242° ESE | 2025-09-14 13:23:51.424Z | 63.363° ENE | 26.352° | 2025-09-14 13:26:51.424Z | 13.106° NNE |
| 5 mins | 2025-09-14 14:57:51.424Z | 232.867° WSW | 2025-09-14 14:59:51.424Z | 270.881° WNW | 20.372° | 2025-09-14 15:02:51.424Z | 316.353° 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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