DODECAPOLE 2

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite DODECAPOLE 2 at a glance.

Uptime

22037

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: 102.147 minutes

Inclination: 90.0616 deg

SMA: 7238.438 km

Apoapsis: 887.821 km

Periapsis: 832.785 km

RAAN: 23.6755 deg

Eccentricy: 0.0038016

Argument of periapsis: 67.1321 deg

Mean anomaly: 293.3871 deg

Mean motion: 14.0972845 rev/day

Mean motion (dot): 0.00005347 rev/day2

B* drag term: 0.0030209357 1/REarth

Two-line elements (TLE)

Creation date: Dec. 12, 2025, 10:14 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Dec. 12, 2025, 3 a.m. UTC

TLE line 0: 0 DODECAPOLE 2

TLE line 1: 1 01510U 65065C 25346.12527057 .00005347 00000-0 30209-2 0 9993

TLE line 2: 2 01510 90.0616 23.6755 0038016 67.1321 293.3871 14.09728450 6792

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.

Target Orbit TCA Probability of collision Miss distance Type
COSMOS 2219 LEO 2025-12-13 04:29:41 0.0006141161 833.0 (m) PAYLOAD
FENGYUN 1C DEB SSO 2025-11-18 12:10:48 0.0001068113 425.0 (m) DEBRIS
CZ-6A DEB LEO 2025-10-13 04:28:41 0.000109866 198.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-08-10 21:37:04 0.0001834155 478.0 (m) DEBRIS
THORAD AGENA D DEB SSO 2025-06-08 07:39:18 0.0002301713 587.0 (m) DEBRIS

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.

Launch to space Thor DM-21 Ablestar | Transit-O 5
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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