ZK-2 R/B, 68413 (Decayed)
Orbit data source: Space-Track
ZK-2 R/B, 68413 was space debris in LEO originally from a launch on Mon, 30 Mar 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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68413 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Zhongke TJ YG
Mission
Decayed spacecraft
Bus & Motor
LK-2 S1, Unknown motor
Mass
17,000 kg wet, 17,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 8.0 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 ZK-2 R/B
1 68413U 26066B 26103.04709367 .25197579 -27237-5 17149-3 0 9997
2 68413 84.6472 267.9233 0071312 162.3208 310.9433 16.45102865 2107Epoch: 2026-04-13T01:07Z
TLE epoch observation values (Epoch: 2026-04-13T01:07:48.893Z)
Latitude
66.8568°
Longitude
-142.86192°
Altitude
133.584 km
Speed
7.851 km/s
True Right ascension
05h 01m 20s
True Declination
66° 43' 13"
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
07:20:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
195.53 km
Perigee altitude
102.438 km
Semi-major axis
6,527.121 km
Eccentricity
0.00713
Inclination
84.6472°
RAAN
267.9233°
Arg. of periapsis
162.3208°
True anomaly
310.32243°
Mean anomaly
310.9433°
Eccentric anomaly
310.63323°
Mean motion
4.11586 °/min
Orbital period
87.47 mins
BSTAR
0.00017149
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Other satellites on launch #66 in the year 2026 (2026-03-30 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.ZK-2 R/B Visibility
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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. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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