GGSE 3

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite GGSE 3 at a glance.

Uptime

21977

Days in orbit

Revolutions

≈ 14.0

Per day

Orbit

LEO

Low Earth Orbit

Inclination

70.1

Latest

Satellite identification and parameters

Extended collection of information and parameters for GGSE 3.

Object identification

Identified? True

Debris? False

Object name: GGSE 3

International designator: 1965-016C

Object number (NORAD): 1292

Object ID (CCSDS): 1292

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 102.753 minutes

Inclination: 70.0752 deg

SMA: 7267.035 km

Apoapsis: 901.757 km

Periapsis: 876.042 km

RAAN: 101.8939 deg

Eccentricy: 0.0017693

Argument of periapsis: 131.7807 deg

Mean anomaly: 228.4817 deg

Mean motion: 14.01415484 rev/day

Mean motion (dot): 0.0000017 rev/day2

B* drag term: 0.00014745 1/REarth

Two-line elements (TLE)

Creation date: May 9, 2025, 2:46 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 8, 2025, 8:07 a.m. UTC

TLE line 0: 0 GGSE 3

TLE line 1: 1 01292U 65016C 25128.33844882 .00000170 00000-0 14745-3 0 9992

TLE line 2: 2 01292 70.0752 101.8939 0017693 131.7807 228.4817 14.01415484 67840

Live tracking on map

Real-time ground track for satellite GGSE 3.

In-orbit conjunctions

A list of the most updated potential collisions computed for object GGSE 3.

Target Orbit TCA Probability of collision Miss distance Type
SL-14 DEB LEO 2025-03-21 03:45:54 0.0002196244 872.0 (m) DEBRIS
OV1-4 R/B SSO 2024-11-05 07:40:48 0.002332664 122.0 (m) ROCKET BODY
METEOR 1-19 LEO 2024-11-01 14:55:15 0.0007875719 344.0 (m) PAYLOAD
CZ-6A DEB SSO 2024-10-16 10:11:48 0.0001087348 849.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-10-07 04:31:00 0.0002444307 102.0 (m) DEBRIS

Associated space launch

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

GGSE 3 was lifted into orbit during the mission ‘Thor SLV-2 Agena D | Poppy 6A,B,C,D’, on board a Thor SLV-2 Agena D space rocket.

The launch took place on March 9, 1965, 6:29 p.m. from Space Launch Complex 2W.

For more information about the launch, click the button.

Launch to space Thor SLV-2 Agena D | Poppy 6A,B,C,D
Thor SLV-2 Agena D | Poppy 6A,B,C,D

Agency: N/A

Status: Launch Successful

Launch date: March 9, 1965, 6:29 p.m. UTC

Rocket: Thor SLV-2 Agena D

Launch pad: Space Launch Complex 2W

Location: Vandenberg SFB, CA, USA

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