ELEKTRON 3, 829
Orbit data source: Space-Track
ELEKTRON 3, 829 is a payload satellite owned by OKB-1 (CIS) in HEO that was launched on Fri, 10 Jul 1964 UTC via a VOSTOK 8K72 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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829 intel report (Beta)
ELEKTRON 3 details
Identifier | |
Orbit | HEO |
Last TLE update | 18 hours ago |
Origin | |
Manufacturer | OKB-1 |
Mission | Civil Science |
Bus & Motor | OBJECT D, Unknown motor |
Mass | 350 kg wet, 350 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Cyl + 6 Pan, 4 m |
Radar Cross Section | 2.718 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 18 hours ago
0 ELEKTRON 3
1 00829U 64038A 24317.33097075 .00001560 00000-0 45211-3 0 9999
2 00829 60.8105 285.6869 2945837 193.1102 157.3034 9.19181044961882
Epoch: 2024-11-12T07:56Z
Definitive object data (Epoch: 2024-11-12T07:56:35.872Z)
Latitude | -0° |
Longitude | 114.59401° |
Altitude | 5,952.741 km |
Speed | 4.823 km/s |
True Right ascension | 19h 02m 44s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -2.57186° |
Longitude | 112.11256° |
Altitude | 5,883.135 km |
Speed | 4.861 km/s |
Apparent Right ascension | 17h 19m 57s |
Apparent Declination | -23° 52' 56" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 22:41:11 |
Azimuth | 245.578° WSW |
Elevation | -8.148° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 6,083.191 km |
Perigee altitude | 412.018 km |
Semi-major axis | 9,625.742 km |
Eccentricity | 0.2945837 |
Inclination | 60.8105° |
RAAN | 285.6869° |
Arg. of periapsis | 193.1102° |
True anomaly | 166.96563° |
Mean anomaly | 157.3034° |
Eccentric anomaly | 162.4054° |
Mean motion | 2.29822 °/min |
BSTAR | 0.00045211 |
Orbital period | 156.64 mins |
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Other satellites on launch #38 in the year 1964 (1964-07-10 UTC)
ELEKTRON 3, 829 |
ELEKTRON 4, 830 (Decayed) |
ELEKTRON 3 DEB, 831 |
SL-3 R/B, 832 (Decayed) |
ELEKTRON 3 DEB, 5892 (Decayed) |
ELEKTRON 3 DEB, 5893 (Decayed) |
ELEKTRON 3 DEB, 29008 |
ELEKTRON 3 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. |
---|---|---|---|---|---|---|---|
49 mins | 2024-11-13 02:27:53.614Z | 257.047° W | 2024-11-13 03:00:53.614Z | 327.856° NNW | 36.388° | 2024-11-13 03:16:53.614Z | 42.225° NE |
26 mins | 2024-11-13 05:35:53.614Z | 308.523° NW | 2024-11-13 05:52:53.614Z | 3.367° NNE | 29.867° | 2024-11-13 06:01:53.614Z | 71.565° E |
17 mins | 2024-11-13 08:27:53.614Z | 320.931° NNW | 2024-11-13 08:39:53.614Z | 247.658° W | 44.894° | 2024-11-13 08:44:53.614Z | 147.072° SSE |
46 mins | 2024-11-13 20:28:53.614Z | 141.276° SSE | 2024-11-13 20:54:53.614Z | 96.269° ESE | 25.49° | 2024-11-13 21:14:53.614Z | 52.578° ENE |
60 mins | 2024-11-13 23:01:53.614Z | 198.408° SSW | 2024-11-13 23:38:53.614Z | 117.526° SE | 44.489° | 2024-11-14 00:01:53.614Z | 39.732° NE |
16 mins | 2024-11-14 01:54:53.614Z | 250.498° W | 2024-11-14 02:10:53.614Z | 267.437° W | 28.096° | 2024-11-14 02:10:53.614Z | 267.437° W |
Authenticating...
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