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: 10 hours ago
TLE from 10 hours ago
0 KAZEOSAT 2
1 40010U 14033A 26112.31968225 .00000784 00000-0 96796-4 0 9994
2 40010 97.5446 314.8720 0009531 135.6992 224.4989 14.85402564640669Epoch: 2026-04-22T07:40Z
TLE epoch observation values (Epoch: 2026-04-22T07:40:20.546Z)
Latitude
0.00005°
Longitude
-10.59643°
Altitude
620.118 km
Speed
7.546 km/s
True Right ascension
20h 59m 29s
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
00:40:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
616 km
Perigee altitude
602.681 km
Semi-major axis
6,987.478 km
Eccentricity
0.00095
Inclination
97.5446°
RAAN
314.872°
Arg. of periapsis
135.6992°
True anomaly
224.42242°
Mean anomaly
224.4989°
Eccentric anomaly
224.46065°
Mean motion
3.71589 °/min
Orbital period
96.88 mins
BSTAR
0.000096796
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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 | 2026-04-23 02:01:19.121Z | 22.684° NE | 2026-04-23 02:05:19.121Z | 110.457° ESE | 38.838° | 2026-04-23 02:08:19.121Z | 174.014° S |
| 6 mins | 2026-04-23 12:55:19.121Z | 125.631° SE | 2026-04-23 12:57:19.121Z | 84.893° E | 29.511° | 2026-04-23 13:01:19.121Z | 7.713° NNE |
| 4 mins | 2026-04-23 14:32:19.121Z | 240.932° WSW | 2026-04-23 14:33:19.121Z | 257.792° W | 17.241° | 2026-04-23 14:36:19.121Z | 306.376° NW |
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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