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DODECAPOLE 2, 1510

Orbit data source: Space-Track

DODECAPOLE 2, 1510 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.

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Identifier
1510, 1965-065C
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
NRL
Mission
Spacecraft
Bus & Motor
NRL 9", 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
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 DODECAPOLE 2
1 01510U 65065C   26202.43964553  .00002263  00000-0  12358-2 0  9994
2 01510  90.0665  25.2525 0040999  76.8144 283.7611 14.11378614 37999
Epoch: 2026-07-21T10:33Z
TLE epoch observation values (Epoch: 2026-07-21T10:33:05.373Z)
Latitude
-0.00002°
Longitude
-72.2292°
Altitude
850.76 km
Speed
7.431 km/s
True Right ascension
01h 41m 00s
True Declination
0° 00' 00"
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
17:21:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
881.26 km
Perigee altitude
821.977 km
Semi-major axis
7,229.756 km
Eccentricity
0.0041
Inclination
90.0665°
RAAN
25.2525°
Arg. of periapsis
76.8144°
True anomaly
283.30422°
Mean anomaly
283.7611°
Eccentric anomaly
283.53271°
Mean motion
3.53067 °/min
Orbital period
101.96 mins
BSTAR
0.0012358
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