CZ-2F DEB, 67719
Orbit data source: Space-Track
CZ-2F DEB, 67719 is space debris in LEO originally from a launch on Sat, 07 Feb 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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67719 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT?
Mission
Spacecraft
Bus & Motor
Unknown
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 CZ-2F DEB
1 67719U 26024F 26104.27816657 .00107498 00000-0 21463-2 0 9996
2 67719 49.7853 209.0288 0262758 56.3259 306.2452 15.16681079 9620Epoch: 2026-04-14T06:40Z
TLE epoch observation values (Epoch: 2026-04-14T06:40:33.591Z)
Latitude
-0°
Longitude
-93.56788°
Altitude
412.479 km
Speed
7.722 km/s
True Right ascension
13h 56m 06s
True Declination
0° 00' 00"
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
19:34:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
697.852 km
Perigee altitude
335.518 km
Semi-major axis
6,894.822 km
Eccentricity
0.02628
Inclination
49.7853°
RAAN
209.0288°
Arg. of periapsis
56.3259°
True anomaly
303.76958°
Mean anomaly
306.2452°
Eccentric anomaly
305.01216°
Mean motion
3.79104 °/min
Orbital period
94.96 mins
BSTAR
0.0021463
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Other satellites on launch #24 in the year 2026 (2026-02-07 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-2F 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-14 15:01:26.553Z | 347.206° N | 2026-04-14 15:02:26.553Z | 16.254° NNE | 22.766° | 2026-04-14 15:05:26.553Z | 80.247° E |
| 4 mins | 2026-04-14 16:40:26.553Z | 279.624° WNW | 2026-04-14 16:41:26.553Z | 241.714° WSW | 38.02° | 2026-04-14 16:44:26.553Z | 143.562° SSE |
| 4 mins | 2026-04-15 09:45:26.553Z | 222.266° SW | 2026-04-15 09:47:26.553Z | 108.054° ESE | 40.902° | 2026-04-15 09:49:26.553Z | 62.658° ENE |
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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