CHOMPTT, 43855 (Decayed)
Orbit data source: Space-Track
CHOMPTT, 43855 was a payload satellite owned by UFla (US) in LEO that was launched on Sun, 16 Dec 2018 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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43855 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
UFla
Mission
Decayed Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
3.59 kg wet, 3.59 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 CHOMPTT
1 43855U 18104G 24134.35325181 .12320967 -15037-5 27872-3 0 9992
2 43855 84.9866 294.2530 0011178 259.2513 100.7537 16.45723631302149Epoch: 2024-05-13T08:28Z
TLE epoch observation values (Epoch: 2024-05-13T08:28:40.956Z)
Latitude
-0.00003°
Longitude
-64.50956°
Altitude
155.31 km
Speed
7.812 km/s
True Right ascension
19h 37m 00s
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
18:13:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
154.625 km
Perigee altitude
140.036 km
Semi-major axis
6,525.468 km
Eccentricity
0.00112
Inclination
84.9866°
RAAN
294.253°
Arg. of periapsis
259.2513°
True anomaly
100.87951°
Mean anomaly
100.7537°
Eccentric anomaly
100.81661°
Mean motion
4.11743 °/min
Orbital period
87.43 mins
BSTAR
0.00027872
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Other satellites on launch #104 in the year 2018 (2018-12-16 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.CHOMPTT 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 | 2025-09-14 01:42:24.792Z | 339.407° N | 2025-09-14 01:45:24.792Z | 47.672° ENE | 30.604° | 2025-09-14 01:46:24.792Z | 86.293° E |
| 4 mins | 2025-09-14 18:29:24.792Z | 250.85° W | 2025-09-14 18:30:24.792Z | 317.614° NNW | 41.492° | 2025-09-14 18:33:24.792Z | 11.466° NNE |
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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