KEPLER-4 (ANTILLES), 46499
Orbit data source: Space-Track
KEPLER-4 (ANTILLES), 46499 is a payload satellite owned by Kepler Comms (CA) in SSO that was launched on Mon, 28 Sep 2020 UTC via a SOYUZ-2-1B launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). Payloads include a variety of satellites, spacecraft, and rockets 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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46499 intel report (Beta)
KEPLER-4 (ANTILLES) details
Identifier | |
Orbit | SSO |
Last TLE update | 15 hours ago |
Origin | |
Manufacturer | KEPLER/UTIAS |
Mission | Operational Commercial Communications |
Bus & Motor | CUBESAT 6U, Unknown motor |
Mass | 15 kg wet, 15 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Box + 2 Pan, Unknown HBR |
Radar Cross Section | 0.109 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 15 hours ago
0 KEPLER-4 (ANTILLES)
1 46499U 20068P 24360.91415256 .00067618 00000-0 11822-2 0 9990
2 46499 97.8118 338.4492 0005747 30.9764 329.1824 15.50402348234193
Epoch: 2024-12-25T21:56Z
Definitive object data (Epoch: 2024-12-25T21:56:22.781Z)
Latitude | -0.00003° |
Longitude | -85.54678° |
Altitude | 415.317 km |
Speed | 7.664 km/s |
True Right ascension | 22h 33m 47s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -48.16929° |
Longitude | -76.08913° |
Altitude | 433.142 km |
Speed | 7.651 km/s |
Apparent Right ascension | 23h 54m 47s |
Apparent Declination | -44° 28' 03" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 12:34:50 |
Azimuth | 124.824° SE |
Elevation | -81.305° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 416.397 km |
Perigee altitude | 408.591 km |
Semi-major axis | 6,790.631 km |
Eccentricity | 0.0005747 |
Inclination | 97.8118° |
RAAN | 338.4492° |
Arg. of periapsis | 30.9764° |
True anomaly | 329.14864° |
Mean anomaly | 329.1824° |
Eccentric anomaly | 329.16552° |
Mean motion | 3.87863 °/min |
BSTAR | 0.0011822 |
Orbital period | 92.82 mins |
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Other satellites on launch #68 in the year 2020 (2020-09-28 UTC)
KEPLER-4 (ANTILLES) 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. |
---|---|---|---|---|---|---|---|
5 mins | 2024-12-26 22:51:12.205Z | 172.872° S | 2024-12-26 22:53:12.205Z | 194.743° SSW | 40.719° | 2024-12-26 22:56:12.205Z | 342.973° N |
4 mins | 2024-12-27 11:41:12.205Z | 10.815° NNE | 2024-12-27 11:43:12.205Z | 200.325° SSW | 41.694° | 2024-12-27 11:45:12.205Z | 194.823° SSW |
Authenticating...
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