ZQ-2E R/B, 101070

Orbit data source: Space-Track

ZQ-2E R/B, 101070 is space debris in SSO originally from a launch on Wed, 14 Oct 2026 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
101070, 2026-234L
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Flag of CNLandspace (CN)
Manufacturer
Lanjian Hangtian
Mission
Spacecraft
Bus & Motor
ZQ-2 ST 2, Unknown motor
Mass
~5,000 kg wet, ~5,000 kg dry
Launch date (UTC)
2026-10-14 (2 days ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 6.0 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 ZQ-2E R/B
1 A1070U 26234L   26289.36559587  .07506387  31862-5  36422-3 0  9991
2 A1070  98.0527 116.2685 0243795   7.9857 352.5185 15.92834540   309
Epoch: 2026-10-16T08:46Z
TLE epoch observation values (Epoch: 2026-10-16T08:46:27.483Z)
Latitude
0.00001°
Longitude
-40.23366°
Altitude
136.27 km
Speed
7.918 km/s
True Right ascension
07h 45m 04s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
17:22:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
453.848 km
Perigee altitude
128.655 km
Semi-major axis
6,669.389 km
Eccentricity
0.02438
Inclination
98.0527°
RAAN
116.2685°
Arg. of periapsis
7.9857°
True anomaly
352.14343°
Mean anomaly
352.5185°
Eccentric anomaly
352.33212°
Mean motion
3.98487 °/min
Orbital period
90.34 mins
BSTAR
0.00036422
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