YZ-1S R/B, 60326

Orbit data source: Space-Track

YZ-1S R/B, 60326 is space debris in HEO originally from a launch on Wed, 13 Mar 2024 UTC launched from the Xichang Space Center, China (XSC). 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
60326, 2024-048E
Orbit
HEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
YZ-1, Unknown motor
Mass
~2,500 kg wet, ~2,500 kg dry
Launch date (UTC)
2024-03-13 (2 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Double Cone, 2.0 m
Radar Cross Section
5.890 m²

Expand to show TLE details & history
Last TLE update: 4 hours ago

TLE from 4 hours ago
0 YZ-1S R/B
1 60326U 24048E   26171.68795945 -.00000408  00000-0  26932-2 0  9992
2 60326  15.9818 302.5650 8933998 246.3067   0.3688  0.47343613  3750
Epoch: 2026-06-20T16:30Z
TLE epoch observation values (Epoch: 2026-06-20T16:30:39.696Z)
Latitude
-14.7343°
Longitude
31.8414°
Altitude
1,271.4 km
Speed
9.924 km/s
True Right ascension
12h 33m 37s
True Declination
-14° 39' 20"
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
07:18:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
125,298.532 km
Perigee altitude
1,035.384 km
Semi-major axis
69,545.095 km
Eccentricity
0.8934
Inclination
15.9818°
RAAN
302.565°
Arg. of periapsis
246.3067°
True anomaly
14.43498°
Mean anomaly
0.3688°
Eccentric anomaly
3.4423°
Mean motion
0.11834 °/min
Orbital period
3,042 mins
BSTAR
0.0026932
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Other satellites on launch #48 in the year 2024 (2024-03-13 UTC)

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