Showing default

CALSPHERE 4(A), 1520

Orbit data source: Space-Track

CALSPHERE 4(A), 1520 is a payload satellite owned by NRL (US) in LEO that was launched on Fri, 13 Aug 1965 UTC via a THOR ABLESTAR 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
1520, 1965-065H
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
NRL
Mission
Operational spacecraft
Bus & Motor
NRL 14", Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
1965-08-13 (61 years ago)
Launch vehicle
THOR ABLESTAR
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
SPHERE, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 CALSPHERE 4(A)
1 01520U 65065H   26236.65719081  .00000072  00000-0  12195-3 0  9996
2 01520  89.8944 121.8068 0067906 270.8518 120.7091 13.36288320971853
Epoch: 2026-08-24T15:46Z
TLE epoch observation values (Epoch: 2026-08-24T15:46:21.285Z)
Latitude
32.2823°
Longitude
-87.65126°
Altitude
1,153.603 km
Speed
7.266 km/s
True Right ascension
08h 07m 29s
True Declination
32° 08' 07"
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
18:55:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,171.125 km
Perigee altitude
1,069.289 km
Semi-major axis
7,498.344 km
Eccentricity
0.00679
Inclination
89.8944°
RAAN
121.8068°
Arg. of periapsis
270.8518°
True anomaly
121.37522°
Mean anomaly
120.7091°
Eccentric anomaly
121.04245°
Mean motion
3.34268 °/min
Orbital period
107.7 mins
BSTAR
0.00012195
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
|