ZK-2 R/B, 68413
Orbit data source: Space-Track
ZK-2 R/B, 68413 is 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
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 2 hours ago
TLE from 2 hours ago
0 ZK-2 R/B
1 68413U 26066B 26102.48615720 .13087951 -27292-5 26118-3 0 9999
2 68413 84.6517 268.3926 0148682 163.4945 257.4755 16.20502707 2010Epoch: 2026-04-12T11:40Z
TLE epoch observation values (Epoch: 2026-04-12T11:40:03.982Z)
Latitude
59.00019°
Longitude
-98.40221°
Altitude
250.958 km
Speed
7.749 km/s
True Right ascension
18h 29m 13s
True Declination
58° 50' 11"
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
20:07:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
312.967 km
Perigee altitude
116.913 km
Semi-major axis
6,593.077 km
Eccentricity
0.01487
Inclination
84.6517°
RAAN
268.3926°
Arg. of periapsis
163.4945°
True anomaly
255.81918°
Mean anomaly
257.4755°
Eccentric anomaly
256.64665°
Mean motion
4.05425 °/min
Orbital period
88.8 mins
BSTAR
0.00026118
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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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| ZK-2 R/B is likely not visible in the next few days. |
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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