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

10098

Days in orbit

Revolutions

≈ 14.5

Per day

Orbit

LEO

Low Earth Orbit

Inclination

86.4

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: 1997-051CB

Object number (NORAD): 33966

Object ID (CCSDS): 33966

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.413 minutes

Inclination: 86.3915 deg

SMA: 7108.66 km

Apoapsis: 735.103 km

Periapsis: 725.947 km

RAAN: 139.8976 deg

Eccentricy: 0.000644

Argument of periapsis: 197.7671 deg

Mean anomaly: 342.1513 deg

Mean motion: 14.48508882 rev/day

Mean motion (dot): 0.00002307 rev/day2

B* drag term: 0.00060953 1/REarth

Two-line elements (TLE)

Creation date: May 8, 2025, 3:01 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 7, 2025, 6:57 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 33966U 97051CB 25127.79003096 .00002307 00000-0 60953-3 0 9998

TLE line 2: 2 33966 86.3915 139.8976 0006440 197.7671 342.1513 14.48508882852716

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
NOAA 16 DEB SSO 2024-11-15 02:02:29 0.0004552588 678.0 (m) DEBRIS
CZ-4 DEB SSO 2024-11-09 15:35:16 0.0001604712 873.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-10-05 01:05:58 0.0001258996 312.0 (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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