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: 5 hours ago
TLE from 5 hours ago
0 KAZEOSAT 2
1 40010U 14033A 26035.52240896 .00001166 00000-0 14157-3 0 9993
2 40010 97.5486 242.0594 0009695 44.0367 316.1619 14.85278975629263Epoch: 2026-02-04T12:32Z
TLE epoch observation values (Epoch: 2026-02-04T12:32:16.134Z)
Latitude
-0.00005°
Longitude
-80.6956°
Altitude
610.863 km
Speed
7.556 km/s
True Right ascension
16h 08m 14s
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
19:46:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
616.503 km
Perigee altitude
602.954 km
Semi-major axis
6,987.866 km
Eccentricity
0.00097
Inclination
97.5486°
RAAN
242.0594°
Arg. of periapsis
44.0367°
True anomaly
316.08488°
Mean anomaly
316.1619°
Eccentric anomaly
316.1234°
Mean motion
3.71558 °/min
Orbital period
96.89 mins
BSTAR
0.00014157
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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 | 2026-02-05 02:03:02.708Z | 32.564° NE | 2026-02-05 02:06:02.708Z | 92.697° ESE | 33.08° | 2026-02-05 02:10:02.708Z | 168.142° S |
| 5 mins | 2026-02-05 12:57:02.708Z | 109.658° ESE | 2026-02-05 12:59:02.708Z | 66.627° ENE | 24.56° | 2026-02-05 13:02:02.708Z | 15.606° NNE |
| 5 mins | 2026-02-05 14:33:02.708Z | 229.459° WSW | 2026-02-05 14:35:02.708Z | 269.203° W | 21.691° | 2026-02-05 14:38:02.708Z | 317.157° 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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