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

20652

Days in orbit

Revolutions

≈ 14.3

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.8

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: 1968-092B

Object number (NORAD): 3522

Object ID (CCSDS): 3522

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 100.644 minutes

Inclination: 98.7598 deg

SMA: 7167.259 km

Apoapsis: 809.061 km

Periapsis: 769.187 km

RAAN: 270.1955 deg

Eccentricy: 0.0027817

Argument of periapsis: 273.5474 deg

Mean anomaly: 86.2527 deg

Mean motion: 14.30780847 rev/day

Mean motion (dot): 0.0000029 rev/day2

B* drag term: 0.00012776 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, 7:47 p.m. UTC

TLE line 0: 0 THOR BURNER 2 R/B

TLE line 1: 1 03522U 68092B 25127.82464938 .00000290 00000-0 12776-3 0 9995

TLE line 2: 2 03522 98.7598 270.1955 0027817 273.5474 86.2527 14.30780847942306

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
ORBCOMM FM 16 DEB LEO 2025-03-02 10:04:00 0.000117704 595.0 (m) DEBRIS
CZ-6A DEB LEO 2025-01-09 02:31:30 0.0001060996 407.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-01-02 05:13:42 0.0002740119 168.0 (m) DEBRIS
CZ-6A DEB LEO 2024-12-11 20:07:35 0.0001323642 924.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-10-29 22:15:06 0.0005094814 274.0 (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 F2’, on board a Thor Burner 2 space rocket.

The launch took place on Oct. 23, 1968, 4:34 a.m. from Space Launch Complex 10W.

For more information about the launch, click the button.

Launch to space Thor Burner 2 | DSAP-4B F2
Thor Burner 2 | DSAP-4B F2

Agency: N/A

Status: Launch Successful

Launch date: Oct. 23, 1968, 4:34 a.m. UTC

Rocket: Thor Burner 2

Launch pad: Space Launch Complex 10W

Location: Vandenberg SFB, CA, USA

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