Showing default

NOAA 4, 7529

Orbit data source: Space-Track

NOAA 4, 7529 is a payload satellite owned by NOAA (US) in SSO that was launched on Fri, 15 Nov 1974 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
7529, 1974-089A
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
RCA/East Windsor
Mission
Non-operational spacecraft
Bus & Motor
TIROS M, Unknown motor
Mass
345 kg wet, 345 kg dry
Launch date (UTC)
1974-11-15 (51 years ago)
Launch vehicle
DELTA 2310
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 NOAA 4
1 07529U 74089A   25287.94033897 -.00000024  00000-0  14074-3 0  9994
2 07529 102.0091 293.1325 0008845 306.0517  83.5534 12.53197323328805
Epoch: 2025-10-14T22:34Z
TLE epoch observation values (Epoch: 2025-10-14T22:34:05.287Z)
Latitude
29.03864°
Longitude
-75.86014°
Altitude
1,453.684 km
Speed
7.138 km/s
True Right ascension
19h 05m 32s
True Declination
28° 54' 21"
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
05:51:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,455.631 km
Perigee altitude
1,441.785 km
Semi-major axis
7,826.845 km
Eccentricity
0.00088
Inclination
102.0091°
RAAN
293.1325°
Arg. of periapsis
306.0517°
True anomaly
83.65413°
Mean anomaly
83.5534°
Eccentric anomaly
83.60376°
Mean motion
3.13446 °/min
Orbital period
114.85 mins
BSTAR
0.00014074
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
|