THOR BURNER 2 R/B

Satellite information

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Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite THOR BURNER 2 R/B at a glance.

Uptime

21138

Days in orbit

Revolutions

≈ 14.2

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.5

Latest

Satellite identification and parameters

Extended collection of information and parameters for THOR BURNER 2 R/B.

Object identification

Identified? True

Debris? False

Object name: THOR BURNER 2 R/B

International designator: 1967-080B

Object number (NORAD): 2940

Object ID (CCSDS): 2940

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 101.614 minutes

Inclination: 98.5455 deg

SMA: 7213.204 km

Apoapsis: 862.75 km

Periapsis: 807.388 km

RAAN: 22.7057 deg

Eccentricy: 0.0038375

Argument of periapsis: 122.4597 deg

Mean anomaly: 238.0297 deg

Mean motion: 14.17132438 rev/day

Mean motion (dot): 0.00000071 rev/day2

B* drag term: 0.000055497 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, 12:52 p.m. UTC

TLE line 0: 0 THOR BURNER 2 R/B

TLE line 1: 1 02940U 67080B 25187.53617638 .00000071 00000-0 55497-4 0 9990

TLE line 2: 2 02940 98.5455 22.7057 0038375 122.4597 238.0297 14.17132438986022

Live tracking on map

Real-time ground track for satellite THOR BURNER 2 R/B.

In-orbit conjunctions

A list of the most updated potential collisions computed for object THOR BURNER 2 R/B.

Target Orbit TCA Probability of collision Miss distance Type
METEOR 2-8 DEB LEO 2025-06-14 10:54:36 0.0008160228 146.0 (m) DEBRIS
DMSP 5D-2 F13 DEB SSO 2025-04-20 15:30:56 0.0001489908 156.0 (m) DEBRIS
CZ-6A DEB LEO 2024-12-06 15:45:46 0.0009019625 383.0 (m) DEBRIS
CZ-6A DEB LEO 2024-11-27 23:15:20 0.0001166117 516.0 (m) DEBRIS
METEOR 1-17 DEB LEO 2024-08-05 12:19:19 0.0009578397 118.0 (m) DEBRIS

Associated space launch

DSAP-4A (Defense Satellite Application Program Block 4A) was the fourth version of the military meteorological satellites of the Defense Meteorological Satellite Program.

THOR BURNER 2 R/B was lifted into orbit during the mission ‘Thor Burner 2 | DSAP-4A F3’, on board a Thor Burner 2 space rocket.

The launch took place on Aug. 23, 1967, 4:41 a.m. from Space Launch Complex 10W.

For more information about the launch, click the button.

Launch to space Thor Burner 2 | DSAP-4A F3
Thor Burner 2 | DSAP-4A F3

Agency: N/A

Status: Launch Successful

Launch date: Aug. 23, 1967, 4:41 a.m. UTC

Rocket: Thor Burner 2

Launch pad: Space Launch Complex 10W

Location: Vandenberg SFB, CA, USA

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