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

≈ 14.4

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: 1997-051VQ

Object number (NORAD): 36083

Object ID (CCSDS): 36083

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.846 minutes

Inclination: 86.3411 deg

SMA: 7129.301 km

Apoapsis: 768.804 km

Periapsis: 733.528 km

RAAN: 129.4061 deg

Eccentricy: 0.002474

Argument of periapsis: 235.7308 deg

Mean anomaly: 124.1549 deg

Mean motion: 14.42222764 rev/day

Mean motion (dot): 0.00002345 rev/day2

B* drag term: 0.00070362 1/REarth

Two-line elements (TLE)

Creation date: May 6, 2025, 3:54 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 5, 2025, 7:40 a.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 36083U 97051VQ 25125.31949201 .00002345 00000-0 70362-3 0 9991

TLE line 2: 2 36083 86.3411 129.4061 0024740 235.7308 124.1549 14.42222764822577

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
FENGYUN 1C DEB SSO 2025-02-28 20:13:50 0.0001448045 381.0 (m) DEBRIS
CZ-6A DEB LEO 2025-01-27 21:43:03 0.005059202 58.0 (m) DEBRIS

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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