TIMATION 1

Satellite information

Favourite Embed

Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite TIMATION 1 at a glance.

Uptime

21381

Days in orbit

Revolutions

≈ 14.0

Per day

Orbit

LEO

Low Earth Orbit

Inclination

70.0

Latest

Satellite identification and parameters

Extended collection of information and parameters for TIMATION 1.

Object identification

Identified? True

Debris? False

Object name: TIMATION 1

International designator: 1967-053E

Object number (NORAD): 2847

Object ID (CCSDS): 2847

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 102.645 minutes

Inclination: 69.9653 deg

SMA: 7261.937 km

Apoapsis: 890.516 km

Periapsis: 877.087 km

RAAN: 252.2608 deg

Eccentricy: 0.00092459

Argument of periapsis: 295.7258 deg

Mean anomaly: 64.2896 deg

Mean motion: 14.0289148 rev/day

Mean motion (dot): 0.00000343 rev/day2

B* drag term: 0.00025601719 1/REarth

Two-line elements (TLE)

Creation date: Dec. 12, 2025, 10:14 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Dec. 12, 2025, 4:47 a.m. UTC

TLE line 0: 0 TIMATION 1

TLE line 1: 1 02847U 67053E 25346.19990262 .00000343 00000-0 25602-3 0 9998

TLE line 2: 2 02847 69.9653 252.2608 0009246 295.7258 64.2896 14.02891480987562

Live tracking on map

Real-time ground track for satellite TIMATION 1.

In-orbit conjunctions

A list of the most updated potential collisions computed for object TIMATION 1.

Target Orbit TCA Probability of collision Miss distance Type
COSMOS 1275 DEB LEO 2025-11-14 20:51:11 0.0002955871 499.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-05-25 05:56:40 0.0001187943 198.0 (m) DEBRIS
METEOR 2-17 DEB LEO 2025-04-22 19:08:16 0.0002940142 47.0 (m) DEBRIS
CZ-6A DEB SSO 2025-01-24 05:54:27 0.0001265681 831.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-11-20 18:41:54 0.0007343895 201.0 (m) DEBRIS

Associated space launch

Poppy was the follow-on ELINT system, which succeeded the Grab ELINT satellite system.

TIMATION 1 was lifted into orbit during the mission ‘Thor SLV-2 Agena D | Poppy 7A,B,C,D’, on board a Thor SLV-2 Agena D space rocket.

The launch took place on May 31, 1967, 9:30 a.m. from Space Launch Complex 2W.

For more information about the launch, click the button.

Launch to space Thor SLV-2 Agena D | Poppy 7A,B,C,D
Thor SLV-2 Agena D | Poppy 7A,B,C,D

Agency: N/A

Status: Launch Successful

Launch date: May 31, 1967, 9:30 a.m. UTC

Rocket: Thor SLV-2 Agena D

Launch pad: Space Launch Complex 2W

Location: Vandenberg SFB, CA, USA

...

Latest news about this satellite

There are no fresh news available about this satellite. Check back as we update our databases every day.


Newsletter sign-up

Weekly statistics, charts and insights to help you stay on top of the space industry.