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

10096

Days in orbit

Revolutions

≈ 14.5

Per day

Orbit

LEO

Low Earth Orbit

Inclination

86.3

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: 1997-051AAB

Object number (NORAD): 38474

Object ID (CCSDS): 38474

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.349 minutes

Inclination: 86.3402 deg

SMA: 7105.639 km

Apoapsis: 747.936 km

Periapsis: 707.072 km

RAAN: 106.7288 deg

Eccentricy: 0.0028755

Argument of periapsis: 107.7397 deg

Mean anomaly: 252.6949 deg

Mean motion: 14.49432739 rev/day

Mean motion (dot): 0.00003319 rev/day2

B* drag term: 0.00085794 1/REarth

Two-line elements (TLE)

Creation date: May 5, 2025, 2:11 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 4, 2025, 4:19 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 38474U 97051AAB 25124.68048119 .00003319 00000-0 85794-3 0 9991

TLE line 2: 2 38474 86.3402 106.7288 0028755 107.7397 252.6949 14.49432739621006

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 2025-01-22 12:20:19 0.0001813026 424.0 (m) DEBRIS
COSMOS 1331 LEO 2024-06-16 17:08:03 0.0007584958 98.0 (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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