CZ-4 DEB, 26168
Orbit data source: Space-Track
CZ-4 DEB, 26168 is space debris in SSO originally from a launch on Thu, 14 Oct 1999 UTC launched from the Taiyaun Space Center, China (TSC). 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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26168 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 CZ-4 DEB
1 26168U 99057BE 25300.04747806 .00000394 00000-0 14496-3 0 9992
2 26168 98.8269 335.1806 0101191 270.9305 118.0849 14.35642411340405Epoch: 2025-10-27T01:08Z
TLE epoch observation values (Epoch: 2025-10-27T01:08:22.104Z)
Latitude
29.69126°
Longitude
-82.61929°
Altitude
811.284 km
Speed
7.432 km/s
True Right ascension
22h 00m 30s
True Declination
29° 32' 41"
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
17:42:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
842.409 km
Perigee altitude
697.742 km
Semi-major axis
7,148.212 km
Eccentricity
0.01012
Inclination
98.8269°
RAAN
335.1806°
Arg. of periapsis
270.9305°
True anomaly
119.10182°
Mean anomaly
118.0849°
Eccentric anomaly
118.59397°
Mean motion
3.59126 °/min
Orbital period
100.24 mins
BSTAR
0.00014496
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Other satellites on launch #57 in the year 1999 (1999-10-14 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.CZ-4 DEB Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-10-28 02:12:21.819Z | 155.263° SSE | 2025-10-28 02:17:21.819Z | 37.998° NE | 42.603° | 2025-10-28 02:21:21.819Z | 352.182° N |
| 6 mins | 2025-10-28 14:25:21.819Z | 55.954° ENE | 2025-10-28 14:28:21.819Z | 102.806° ESE | 22.579° | 2025-10-28 14:31:21.819Z | 142.87° SSE |
| 8 mins | 2025-10-28 16:03:21.819Z | 352.588° N | 2025-10-28 16:07:21.819Z | 283.104° WNW | 32.794° | 2025-10-28 16:11:21.819Z | 225.675° WSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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