YAOGAN 30 DEB, 42676

Orbit data source: Space-Track

YAOGAN 30 DEB, 42676 is space debris in SSO originally from a launch on Sun, 15 May 2016 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
42676, 2016-029B
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2016-05-15 (10 years ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 YAOGAN 30 DEB
1 42676U 16029B   26171.47215978  .00001389  00000-0  39879-3 0  9993
2 42676  98.0388 357.9399 0233103  85.9828 276.7965 14.31598876512530
Epoch: 2026-06-20T11:19Z
TLE epoch observation values (Epoch: 2026-06-20T11:19:54.604Z)
Latitude
-0.00004°
Longitude
-80.72391°
Altitude
773.43 km
Speed
7.476 km/s
True Right ascension
23h 51m 45s
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
21:27:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
950.441 km
Perigee altitude
616.561 km
Semi-major axis
7,161.638 km
Eccentricity
0.02331
Inclination
98.0388°
RAAN
357.9399°
Arg. of periapsis
85.9828°
True anomaly
274.13589°
Mean anomaly
276.7965°
Eccentric anomaly
275.46699°
Mean motion
3.58117 °/min
Orbital period
100.53 mins
BSTAR
0.00039879
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Other satellites on launch #29 in the year 2016 (2016-05-15 UTC)

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