ECHO 1 DEB (METAL OBJ)

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite ECHO 1 DEB (METAL OBJ) at a glance.

Uptime

23593

Days in orbit

Revolutions

≈ 12.2

Per day

Orbit

LEO

Low Earth Orbit

Inclination

47.3

Latest

Satellite identification and parameters

Extended collection of information and parameters for ECHO 1 DEB (METAL OBJ).

Object identification

Identified? True

Debris? True

Object name: ECHO 1 DEB (METAL OBJ)

International designator: 1960-009E

Object number (NORAD): 53

Object ID (CCSDS): 53

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 118.287 minutes

Inclination: 47.2784 deg

SMA: 7982.138 km

Apoapsis: 1682.188 km

Periapsis: 1525.819 km

RAAN: 313.8376 deg

Eccentricy: 0.0097949

Argument of periapsis: 162.6544 deg

Mean anomaly: 197.7628 deg

Mean motion: 12.17373603 rev/day

Mean motion (dot): -0.00000043 rev/day2

B* drag term: 0.0004068 1/REarth

Two-line elements (TLE)

Creation date: March 16, 2025, 6:34 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: March 16, 2025, 2:21 p.m. UTC

TLE line 0: 0 ECHO 1 DEB (METAL OBJ)

TLE line 1: 1 00053U 60009E 25075.59797130 -.00000043 00000-0 40680-3 0 9992

TLE line 2: 2 00053 47.2784 313.8376 0097949 162.6544 197.7628 12.17373603879680

Live tracking on map

Real-time ground track for satellite ECHO 1 DEB (METAL OBJ).

Associated space launch

The Echo 1A spacecraft was a 30.48 m diameter balloon of mylar polyester film 0.0127 mm thick. The spacecraft was designed as a passive communications reflector for transcontinental and intercontinental telephone (voice), radio, and television signals. It had 107.9 MHz beacon transmitters for telemetry purposes. These transmitters were powered by five nickel-cadmium batteries that were charged by 70 solar cells mounted on the balloon. Because of the large area-to-mass ratio of the spacecraft, data for the calculation of atmospheric density and solar pressure could be acquired. The spacecraft was also used to evaluate the technical feasibility of satellite triangulation during the latter portion of its life. Echo 1 failed during the coast period after launch, as the attitude control jets on the second stage failed and the spacecraft did not achieve orbit. Echo 1A was a successful relaunch.

ECHO 1 DEB (METAL OBJ) was lifted into orbit during the mission ‘Thor Delta | Echo 1’, on board a Thor Delta space rocket.

The launch took place on Aug. 12, 1960, 9:39 a.m. from Space Launch Complex 17A.

For more information about the launch, click the button.

Launch to space Thor Delta | Echo 1
Thor Delta | Echo 1

Agency: N/A

Status: Launch Successful

Launch date: Aug. 12, 1960, 9:39 a.m. UTC

Rocket: Thor Delta

Launch pad: Space Launch Complex 17A

Location: Cape Canaveral SFS, FL, USA

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