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

21537

Days in orbit

Revolutions

≈ 14.5

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.2

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: 1966-082B

Object number (NORAD): 2422

Object ID (CCSDS): 2422

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 99.557 minutes

Inclination: 98.2084 deg

SMA: 7115.556 km

Apoapsis: 816.214 km

Periapsis: 658.628 km

RAAN: 43.96 deg

Eccentricy: 0.01107333

Argument of periapsis: 4.1357 deg

Mean anomaly: 356.0724 deg

Mean motion: 14.46403603 rev/day

Mean motion (dot): 0.00000659 rev/day2

B* drag term: 0.00018223367 1/REarth

Two-line elements (TLE)

Creation date: Sept. 3, 2025, 2:21 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Sept. 2, 2025, 10:35 p.m. UTC

TLE line 0: 0 THOR BURNER 2 R/B

TLE line 1: 1 02422U 66082B 25245.94118692 .00000659 00000-0 18223-3 0 9999

TLE line 2: 2 02422 98.2084 43.9600 0110733 4.1357 356.0724 14.46403603 73749

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 2251 DEB LEO 2025-08-01 12:09:41 0.0001877897 257.0 (m) DEBRIS
NOAA 16 DEB SSO 2025-05-15 02:19:11 0.000103265 488.0 (m) DEBRIS
SL-14 DEB LEO 2025-05-06 08:28:47 0.000175618 511.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-04-20 00:30:08 0.0002518219 294.0 (m) DEBRIS
COSMOS 1375 DEB LEO 2025-03-10 12:58:14 0.0003028478 142.0 (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 F1’, on board a Thor Burner 2 space rocket.

The launch took place on Sept. 16, 1966, 4:36 a.m. from Space Launch Complex 10W.

For more information about the launch, click the button.

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

Agency: N/A

Status: Launch Successful

Launch date: Sept. 16, 1966, 4:36 a.m. UTC

Rocket: Thor Burner 2

Launch pad: Space Launch Complex 10W

Location: Vandenberg SFB, CA, USA

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