IRIDIUM 33 DEB

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite IRIDIUM 33 DEB at a glance.

Uptime

10099

Days in orbit

Revolutions

≈ 14.4

Per day

Orbit

LEO

Low Earth Orbit

Inclination

86.2

Latest

Satellite identification and parameters

Extended collection of information and parameters for IRIDIUM 33 DEB.

Object identification

Identified? True

Debris? True

Object name: IRIDIUM 33 DEB

International designator: 1997-051DY

Object number (NORAD): 34145

Object ID (CCSDS): 34145

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.957 minutes

Inclination: 86.2111 deg

SMA: 7134.598 km

Apoapsis: 797.683 km

Periapsis: 715.243 km

RAAN: 69.6275 deg

Eccentricy: 0.0057775

Argument of periapsis: 92.5915 deg

Mean anomaly: 268.19 deg

Mean motion: 14.40616894 rev/day

Mean motion (dot): 0.00003988 rev/day2

B* drag term: 0.0012203 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, 6:33 a.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 34145U 97051DY 25128.27311803 .00003988 00000-0 12203-2 0 9990

TLE line 2: 2 34145 86.2111 69.6275 0057775 92.5915 268.1900 14.40616894844910

Live tracking on map

Real-time ground track for satellite IRIDIUM 33 DEB.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 33 DEB.

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB LEO 2025-01-24 23:44:58 0.0001602514 713.0 (m) DEBRIS
CZ-6A DEB LEO 2024-10-22 11:22:09 0.00206175 93.0 (m) DEBRIS
CZ-6A DEB LEO 2024-10-20 18:27:18 0.0001282968 730.0 (m) DEBRIS
CZ-6A DEB LEO 2024-10-10 10:58:27 0.00362287 74.0 (m) DEBRIS
COSMOS 2150 LEO 2024-08-21 23:50:41 0.0001999165 890.0 (m) PAYLOAD

Associated space launch

Iridium provides global mobile telecommunications services using a constellation of 66 low earth orbit satellites in a 86.4° inclined orbit. Although 77 satellites were originally envisioned for the system and spawned the name based on the 77th element in the periodic table, the system has been scaled back. Motorola's Satellite Communications Group designed and manufactured the Iridium satellites with Lockheed Martin providing the LM-700A spacecraft buses.

IRIDIUM 33 DEB was lifted into orbit during the mission ‘Proton-K/17S40 | Iridium 27 to 33’, on board a Proton-K/17S40 space rocket.

The launch took place on Sept. 14, 1997, 1:36 a.m. from 81/23 (81L).

For more information about the launch, click the button.

Launch to space Proton-K/17S40 | Iridium 27 to 33
Proton-K/17S40 | Iridium 27 to 33

Agency: N/A

Status: Launch Successful

Launch date: Sept. 14, 1997, 1:36 a.m. UTC

Rocket: Proton-K/17S40

Launch pad: 81/23 (81L)

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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