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

≈ 14.3

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: 1997-051ZC

Object number (NORAD): 38228

Object ID (CCSDS): 38228

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 100.924 minutes

Inclination: 86.2935 deg

SMA: 7180.51 km

Apoapsis: 848.442 km

Periapsis: 756.308 km

RAAN: 142.3391 deg

Eccentricy: 0.0064156

Argument of periapsis: 180.6111 deg

Mean anomaly: 299.4286 deg

Mean motion: 14.26822035 rev/day

Mean motion (dot): 0.0000107 rev/day2

B* drag term: 0.00042421 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, 8:05 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 38228U 97051ZC 25125.83700296 .00001070 00000-0 42421-3 0 9999

TLE line 2: 2 38228 86.2935 142.3391 0064156 180.6111 299.4286 14.26822035816313

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
COSMOS 1867 LEO 2025-03-16 12:22:14 0.0001177758 596.0 (m) PAYLOAD
CZ-6A DEB LEO 2024-10-10 11:17:02 0.0001996216 742.0 (m) DEBRIS
METEOR 1-19 LEO 2024-06-25 00:58:15 0.0001369242 463.0 (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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