DODECAPOLE 2

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite DODECAPOLE 2 at a glance.

Uptime

21878

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: 102.254 minutes

Inclination: 90.0563 deg

SMA: 7243.469 km

Apoapsis: 891.094 km

Periapsis: 839.574 km

RAAN: 22.6313 deg

Eccentricy: 0.0035563

Argument of periapsis: 204.1593 deg

Mean anomaly: 155.7924 deg

Mean motion: 14.0826008 rev/day

Mean motion (dot): 0.00002753 rev/day2

B* drag term: 0.0015968 1/REarth

Two-line elements (TLE)

Creation date: July 6, 2025, 6:05 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 6, 2025, 2:31 p.m. UTC

TLE line 0: 0 DODECAPOLE 2

TLE line 1: 1 01510U 65065C 25187.60494271 .00002753 00000-0 15968-2 0 9993

TLE line 2: 2 01510 90.0563 22.6313 0035563 204.1593 155.7924 14.08260080984480

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
THORAD AGENA D DEB SSO 2025-06-08 07:39:18 0.0002301713 587.0 (m) DEBRIS
NOAA 13 SSO 2025-06-02 01:13:27 0.0002238879 801.0 (m) PAYLOAD
CZ-6A DEB LEO 2025-05-06 11:21:26 0.0005669549 806.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-12-28 09:57:55 0.0005952382 780.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-12-16 12:53:05 0.0005247276 59.0 (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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