Showing default

NOAA 5, 9057

Orbit data source: Space-Track

NOAA 5, 9057 is a payload satellite owned by NOAA (US) in SSO that was launched on Thu, 29 Jul 1976 UTC via a DELTA 2310 launch vehicle from the Air Force Western Test Range (AFWTR). 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.

Loading next visibility...
Identifier
9057, 1976-077A
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
RCA/East Windsor
Mission
Non-operational Civil Weather
Bus & Motor
TIROS M, Unknown motor
Mass
340 kg wet, 340 kg dry
Launch date (UTC)
1976-07-29 (49 years ago)
Launch vehicle
DELTA 2310
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Hex Poly + 3 Pan, 0.6 m
Radar Cross Section
1.292 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 20 hours ago

TLE from 20 hours ago
0 NOAA 5
1 09057U 76077A   25242.20475955 -.00000021  00000-0  19401-3 0  9992
2 09057 102.2663 221.9373 0009716 149.4360 221.7081 12.37820981218474
Epoch: 2025-08-30T04:54Z
TLE epoch observation values (Epoch: 2025-08-30T04:54:51.225Z)
Latitude
10.77099°
Longitude
167.22255°
Altitude
1,523.374 km
Speed
7.102 km/s
True Right ascension
14h 38m 18s
True Declination
10° 42' 51"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
16:44:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,521.115 km
Perigee altitude
1,505.78 km
Semi-major axis
7,891.584 km
Eccentricity
0.00097
Inclination
102.2663°
RAAN
221.9373°
Arg. of periapsis
149.436°
True anomaly
221.63409°
Mean anomaly
221.7081°
Eccentric anomaly
221.67109°
Mean motion
3.09597 °/min
Orbital period
116.28 mins
BSTAR
0.00019401
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|