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.
Focus sentinelFocus sentinel
61984 intel report (Beta)
CZ-7 R/B details
Identifier | |
Orbit | Decayed |
Last TLE update | 3 weeks ago |
Origin | |
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 | Payload Rocket body Debris |
Shape & HBR | Unknown |
Radar Cross Section | Large (>1 m²) |
Expand to show TLE details & history
TLE from 3 weeks 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 1408
Epoch: 2024-11-24T08:29Z
Definitive object data (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 | Object was in full shadow at TLE epoch |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
Apogee altitude | 175.5 km |
Perigee altitude | 140.064 km |
Semi-major axis | 6,535.919 km |
Eccentricity | 0.0027109 |
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 |
BSTAR | 0.00018818 |
Orbital period | 87.64 mins |
Loading maneuver chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #211 in the year 2024 (2024-11-15 UTC)
TIANZHOU 8, 61983 |
CZ-7 R/B, 61984 (Decayed) |
CZ-7 DEB, 61985 (Decayed) |
CZ-7 DEB, 61986 (Decayed) |
CZ-7 DEB, 61987 (Decayed) |
CZ-7 R/B Visibility forecast
Observer location: undefined°, undefined
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. |
---|
Authenticating...
Click to sort rows by NORAD ID header in ascending order | Click to sort rows by Common name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
---|