CZ-7 R/B, 61984 (Decayed)
Orbit data source: Space-Track
CZ-7 R/B, 61984 was space debris in LEO originally from a launch on Fri, 15 Nov 2024 UTC launched from the Wenchang Satellite Launch Center (WSC). 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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61984 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Decayed spacecraft
Bus & Motor
CZ-7 STAGE 2, Unknown motor
Mass
6,000 kg wet, 6,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 5.8 m
Radar Cross Section
34.665 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 CZ-7 R/B
1 61984U 24211B 24329.35362730 .09040425 80355-5 18818-3 0 9996
2 61984 41.4473 181.8548 0027109 242.9030 295.1652 16.43893066 1408Epoch: 2024-11-24T08:29Z
TLE epoch observation values (Epoch: 2024-11-24T08:29:13.398Z)
Latitude
1.41633°
Longitude
169.16035°
Altitude
147.386 km
Speed
7.824 km/s
True Right ascension
00h 01m 02s
True Declination
1° 24' 25"
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
04:01:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
175.5 km
Perigee altitude
140.064 km
Semi-major axis
6,535.919 km
Eccentricity
0.00271
Inclination
41.4473°
RAAN
181.8548°
Arg. of periapsis
242.903°
True anomaly
294.88363°
Mean anomaly
295.1652°
Eccentric anomaly
295.02446°
Mean motion
4.10755 °/min
Orbital period
87.64 mins
BSTAR
0.00018818
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Other satellites on launch #211 in the year 2024 (2024-11-15 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-7 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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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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