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

20919

Days in orbit

Revolutions

≈ 14.2

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.6

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: 1968-042B

Object number (NORAD): 3271

Object ID (CCSDS): 3271

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 101.587 minutes

Inclination: 98.5585 deg

SMA: 7211.952 km

Apoapsis: 870.404 km

Periapsis: 797.23 km

RAAN: 62.4912 deg

Eccentricy: 0.00507311

Argument of periapsis: 308.053 deg

Mean anomaly: 51.6073 deg

Mean motion: 14.17501564 rev/day

Mean motion (dot): 0.00000179 rev/day2

B* drag term: 0.00010784878 1/REarth

Two-line elements (TLE)

Creation date: Aug. 31, 2025, 2:26 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Aug. 30, 2025, 6:17 p.m. UTC

TLE line 0: 0 THOR BURNER 2 R/B

TLE line 1: 1 03271U 68042B 25242.76190966 .00000179 00000-0 10785-3 0 9993

TLE line 2: 2 03271 98.5585 62.4912 0050731 308.0530 51.6073 14.17501564955672

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
COSMOS 1275 DEB LEO 2025-07-26 21:46:03 0.0003092598 62.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-05-14 09:40:11 0.0002139389 362.0 (m) DEBRIS
CZ-6A DEB SSO 2025-02-06 04:02:42 0.000246549 281.0 (m) DEBRIS
CZ-6A DEB LEO 2025-02-02 00:36:23 0.0002034189 432.0 (m) DEBRIS
CZ-6A DEB SSO 2024-09-12 19:57:48 0.0001409334 136.0 (m) DEBRIS

Associated space launch

DSAP-4B (Defense Satellite Application Program Block 4B) was the sixth 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-4B F1’, on board a Thor Burner 2 space rocket.

The launch took place on May 23, 1968, 4:38 a.m. from Space Launch Complex 10W.

For more information about the launch, click the button.

Launch to space Thor Burner 2 | DSAP-4B F1
Thor Burner 2 | DSAP-4B F1

Agency: N/A

Status: Launch Successful

Launch date: May 23, 1968, 4:38 a.m. UTC

Rocket: Thor Burner 2

Launch pad: Space Launch Complex 10W

Location: Vandenberg SFB, CA, USA

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