CZ-4 DEB, 26127
Orbit data source: Space-Track
CZ-4 DEB, 26127 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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26127 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
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 CZ-4 DEB
1 26127U 99057P 25300.97592848 .00025676 00000-0 29041-2 0 9994
2 26127 98.4313 95.1488 0062367 128.0794 355.8844 14.85013107350148Epoch: 2025-10-27T23:25Z
TLE epoch observation values (Epoch: 2025-10-27T23:25:20.220Z)
Latitude
55.28163°
Longitude
-100.47202°
Altitude
579.214 km
Speed
7.6 km/s
True Right ascension
19h 09m 43s
True Declination
55° 06' 59"
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
00:21:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
654.19 km
Perigee altitude
567.017 km
Semi-major axis
6,988.74 km
Eccentricity
0.00624
Inclination
98.4313°
RAAN
95.1488°
Arg. of periapsis
128.0794°
True anomaly
355.83271°
Mean anomaly
355.8844°
Eccentric anomaly
355.85859°
Mean motion
3.71488 °/min
Orbital period
96.91 mins
BSTAR
0.0029041
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-28 10:18:31.726Z | 161.699° S | 2025-10-28 10:22:31.726Z | 23.555° NE | 44.069° | 2025-10-28 10:25:31.726Z | 349.664° N |
| 5 mins | 2025-10-28 23:42:31.726Z | 350.321° N | 2025-10-28 23:44:31.726Z | 290.485° WNW | 37.129° | 2025-10-28 23:47:31.726Z | 216.853° SW |
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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