Key statistics
Satellite DODECAPOLE 2 at a glance.
Uptime
21934
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
90.1
Latest
Satellite identification and parameters
Extended collection of information and parameters for DODECAPOLE 2.
Object identification
Identified? True
Debris? False
Object name: DODECAPOLE 2
International designator: 1965-065C
Object number (NORAD): 1510
Object ID (CCSDS): 1510
Country: UNITED STATES OF AMERICA (US)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 102.228 minutes
Inclination: 90.0599 deg
SMA: 7242.249 km
Apoapsis: 890.71 km
Periapsis: 837.519 km
RAAN: 22.9859 deg
Eccentricy: 0.00367228
Argument of periapsis: 32.6376 deg
Mean anomaly: 327.7066 deg
Mean motion: 14.08615787 rev/day
Mean motion (dot): 0.00006034 rev/day2
B* drag term: 0.0034820042 1/REarth
Two-line elements (TLE)
Creation date: Sept. 1, 2025, 2:20 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 31, 2025, 10:40 p.m. UTC
TLE line 0: 0 DODECAPOLE 2
TLE line 1: 1 01510U 65065C 25243.94444916 .00006034 00000-0 34820-2 0 9998
TLE line 2: 2 01510 90.0599 22.9859 0036723 32.6376 327.7066 14.08615787992417
Live tracking on map
Real-time ground track for satellite DODECAPOLE 2.
In-orbit conjunctions
A list of the most updated potential collisions computed for object DODECAPOLE 2.
Associated space launch
The Transit-O series of satellites that closely followed the design of Transit 5C-1 were also called “Oscars” (Oscar is the phonetic alphabet for “O”, i. e., operational). They were also called NNS (Navy Navigation Satellite) or shortened NavSat.
DODECAPOLE 2 was lifted into orbit during the mission ‘Thor DM-21 Ablestar | Transit-O 5’, on board a Thor DM-21 Ablestar space rocket.
The launch took place on Aug. 13, 1965, 10:11 p.m. from Space Launch Complex 2E.
For more information about the launch, click the button.
Thor DM-21 Ablestar | Transit-O 5
Agency: N/A
Status: Launch Successful
Launch date: Aug. 13, 1965, 10:11 p.m. UTC
Rocket: Thor DM-21 Ablestar
Launch pad: Space Launch Complex 2E
Location: Vandenberg SFB, CA, USA
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