CZ-2C DEB, 67587

Orbit data source: Space-Track

CZ-2C DEB, 67587 is space debris in SSO originally from a launch on Thu, 15 Jan 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
67587, 2026-009D
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT?
Mission
Spacecraft
Bus & Motor
Unknown
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
2026-01-15 (2 months ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 CZ-2C DEB
1 67587U 26009D   26065.45593715  .00054836  00000-0  24656-2 0  9999
2 67587  97.6671 140.5294 0101141  54.4112 306.6494 15.16373342  7601
Epoch: 2026-03-06T10:56Z
TLE epoch observation values (Epoch: 2026-03-06T10:56:32.969Z)
Latitude
-0.00001°
Longitude
172.20035°
Altitude
478.713 km
Speed
7.649 km/s
True Right ascension
09h 22m 07s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
08:34:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.5 km
Perigee altitude
444.088 km
Semi-major axis
6,891.931 km
Eccentricity
0.01011
Inclination
97.6671°
RAAN
140.5294°
Arg. of periapsis
54.4112°
True anomaly
305.71251°
Mean anomaly
306.6494°
Eccentric anomaly
306.18166°
Mean motion
3.79343 °/min
Orbital period
94.9 mins
BSTAR
0.0024656
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Other satellites on launch #9 in the year 2026 (2026-01-15 UTC)

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