DODECAPOLE 2

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite DODECAPOLE 2 at a glance.

Uptime

21819

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: 102.28 minutes

Inclination: 90.0573 deg

SMA: 7244.695 km

Apoapsis: 896.19 km

Periapsis: 836.929 km

RAAN: 22.2632 deg

Eccentricy: 0.00409

Argument of periapsis: 36.9638 deg

Mean anomaly: 323.4351 deg

Mean motion: 14.07902689 rev/day

Mean motion (dot): 0.00004344 rev/day2

B* drag term: 0.002535 1/REarth

Two-line elements (TLE)

Creation date: May 8, 2025, 3:01 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 7, 2025, 11:36 p.m. UTC

TLE line 0: 0 DODECAPOLE 2

TLE line 1: 1 01510U 65065C 25127.98373792 .00004344 00000-0 25350-2 0 9996

TLE line 2: 2 01510 90.0573 22.2632 0040900 36.9638 323.4351 14.07902689976096

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
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
SL-16 DEB LEO 2024-11-17 20:22:04 0.0001180618 459.0 (m) DEBRIS
COSMOS 1275 DEB LEO 2024-11-10 01:53:30 0.0002882508 662.0 (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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