CZ-4 DEB, 26126
Orbit data source: Space-Track
CZ-4 DEB, 26126 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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26126 intel report (Beta)
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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
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 4 hours ago
TLE from 4 hours ago
0 CZ-4 DEB
1 26126U 99057N 26090.61100052 .00001715 00000-0 47604-3 0 9997
2 26126 98.6376 143.7209 0095032 51.5348 106.5754 14.45220743364552Epoch: 2026-03-31T14:39Z
TLE epoch observation values (Epoch: 2026-03-31T14:39:50.444Z)
Latitude
20.60935°
Longitude
-81.96758°
Altitude
763.78 km
Speed
7.464 km/s
True Right ascension
21h 47m 54s
True Declination
20° 29' 47"
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
00:28:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
806.052 km
Perigee altitude
670.792 km
Semi-major axis
7,116.559 km
Eccentricity
0.0095
Inclination
98.6376°
RAAN
143.7209°
Arg. of periapsis
51.5348°
True anomaly
107.61555°
Mean anomaly
106.5754°
Eccentric anomaly
107.09583°
Mean motion
3.61525 °/min
Orbital period
99.58 mins
BSTAR
0.00047604
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-04-01 03:20:43.473Z | 160.762° S | 2026-04-01 03:24:43.473Z | 114.838° SE | 44.188° | 2026-04-01 03:28:43.473Z | 349.671° N |
| 6 mins | 2026-04-01 15:27:43.473Z | 53.513° ENE | 2026-04-01 15:30:43.473Z | 101.93° ESE | 22.016° | 2026-04-01 15:33:43.473Z | 143.792° SSE |
| 7 mins | 2026-04-01 17:05:43.473Z | 348.002° N | 2026-04-01 17:08:43.473Z | 295.492° NW | 30.554° | 2026-04-01 17:12:43.473Z | 228.775° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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