PROXIMA I, 43694 (Decayed)
Orbit data source: Space-Track
PROXIMA I, 43694 was a payload satellite owned by Fleet Space (AU) in LEO that was launched on Sun, 11 Nov 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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43694 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
AU / AUSRelated business
Manufacturer
Fleet Space
Mission
Decayed Commercial Communications
Bus & Motor
CUBESAT 1.5U, Unknown motor
Mass
2 kg wet, 2 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.026 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 PROXIMA I
1 43694U 18088E 24139.06678571 .11242035 -15002-5 41498-3 0 9991
2 43694 84.9859 193.3122 0011906 260.3583 99.6379 16.43111434308020Epoch: 2024-05-18T01:36Z
TLE epoch observation values (Epoch: 2024-05-18T01:36:10.285Z)
Latitude
-0.00002°
Longitude
-66.96845°
Altitude
162.167 km
Speed
7.808 km/s
True Right ascension
12h 53m 14s
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
09:52:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
162.029 km
Perigee altitude
146.474 km
Semi-major axis
6,532.389 km
Eccentricity
0.00119
Inclination
84.9859°
RAAN
193.3122°
Arg. of periapsis
260.3583°
True anomaly
99.77237°
Mean anomaly
99.6379°
Eccentric anomaly
99.70514°
Mean motion
4.11088 °/min
Orbital period
87.57 mins
BSTAR
0.00041498
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Other satellites on launch #88 in the year 2018 (2018-11-11 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.PROXIMA I 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
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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