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

20437

Days in orbit

Revolutions

≈ 14.3

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.4

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: 1969-062B

Object number (NORAD): 4048

Object ID (CCSDS): 4048

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 100.555 minutes

Inclination: 98.3533 deg

SMA: 7163.01 km

Apoapsis: 814.82 km

Periapsis: 754.929 km

RAAN: 23.0627 deg

Eccentricy: 0.0041806

Argument of periapsis: 16.6929 deg

Mean anomaly: 343.562 deg

Mean motion: 14.32054192 rev/day

Mean motion (dot): 0.00000132 rev/day2

B* drag term: 0.000063963 1/REarth

Two-line elements (TLE)

Creation date: July 5, 2025, 5:45 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 5, 2025, 12:27 p.m. UTC

TLE line 0: 0 THOR BURNER 2 R/B

TLE line 1: 1 04048U 69062B 25186.51930390 .00000132 00000-0 63963-4 0 9998

TLE line 2: 2 04048 98.3533 23.0627 0041806 16.6929 343.5620 14.32054192914986

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
FENGYUN 1C DEB SSO 2025-06-21 18:28:03 0.0002051327 183.0 (m) DEBRIS
DMSP 5D-2 F13 DEB SSO 2025-06-15 19:31:29 0.002945791 17.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-03-31 10:09:49 0.0009018626 282.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-01-22 23:58:11 0.0003552302 134.0 (m) DEBRIS
THOR ABLESTAR DEB LEO 2025-01-03 00:12:36 0.0001684226 466.0 (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 F3’, on board a Thor Burner 2 space rocket.

The launch took place on July 23, 1969, 4:39 a.m. from Space Launch Complex 10W.

For more information about the launch, click the button.

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

Agency: N/A

Status: Launch Successful

Launch date: July 23, 1969, 4:39 a.m. UTC

Rocket: Thor Burner 2

Launch pad: Space Launch Complex 10W

Location: Vandenberg SFB, CA, USA

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