NATO 2A, 4353
Orbit data source: Space-Track
NATO 2A, 4353 is a payload satellite owned by NATO (NATO) in GEO that was launched on Fri, 20 Mar 1970 UTC via a THOR DELTA M launch vehicle from the Air Force Eastern Test Range (AFETR). 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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Edit Public Description
Identifier | |
Orbit | GEO |
Last TLE update | 14 hours ago |
Origin | |
Manufacturer | Philco-Ford |
Mission | Non-operational Defense Communications |
Bus & Motor | SKYNET, STAR 17A |
Mass | 243 kg wet, ~107 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Cyl, 1.4 m |
Radar Cross Section | 1.131 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 14 hours ago
0 NATO 2A
1 04353U 70021A 25070.59289888 -.00000103 00000-0 00000-0 0 9991
2 04353 1.5380 284.5191 0001813 316.4984 36.4017 1.00262092121122
Epoch: 2025-03-11T14:13Z
Definitive object data (Epoch: 2025-03-11T14:13:46.463Z)
Latitude | -0.16918° |
Longitude | -105.46665° |
Altitude | 35,782.717 km |
Speed | 3.075 km/s |
True Right ascension | 18h 29m 52s |
True Declination | 0° 10' 08" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -0.71408° |
Longitude | 108.85822° |
Altitude | 35,791.38 km |
Speed | 3.074 km/s |
Apparent Right ascension | 08h 46m 57s |
Apparent Declination | -7° 01' 49" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 08:48:49 |
Azimuth | 180.633° SSW |
Elevation | 43.052° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 35,798.027 km |
Perigee altitude | 35,782.737 km |
Semi-major axis | 42,168.519 km |
Eccentricity | 0.0001813 |
Inclination | 1.538° |
RAAN | 284.5191° |
Arg. of periapsis | 316.4984° |
True anomaly | 36.41403° |
Mean anomaly | 36.4017° |
Eccentric anomaly | 36.40787° |
Mean motion | 0.25065 °/min |
BSTAR | Unknown |
Orbital period | 1436.29 mins |
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4353 neighbors
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Other satellites on launch #21 in the year 1970 (1970-03-20 UTC)
DELTA 1 R/B, 4354 |
DELTA 1 DEB, 5975 |
NATO 2A 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. |
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1440 mins | 2025-03-12 04:28:59.087Z | 180.632° SSW | 2025-03-12 20:38:59.087Z | 180.634° SSW | 35.514° | 2025-03-13 04:28:59.087Z | 180.69° SSW |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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