ALOS DEB

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite ALOS DEB at a glance.

Uptime

7105

Days in orbit

Revolutions

≈ 14.8

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.0

Latest

Satellite identification and parameters

Extended collection of information and parameters for ALOS DEB.

Object identification

Identified? True

Debris? True

Object name: ALOS DEB

International designator: 2006-002AA

Object number (NORAD): 36571

Object ID (CCSDS): 36571

Country: JAPAN (JPN)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 97.208 minutes

Inclination: 98.0003 deg

SMA: 7003.183 km

Apoapsis: 625.73 km

Periapsis: 624.366 km

RAAN: 154.8736 deg

Eccentricy: 0.0000974

Argument of periapsis: 106.1028 deg

Mean anomaly: 254.0292 deg

Mean motion: 14.8135643 rev/day

Mean motion (dot): 0.00003056 rev/day2

B* drag term: 0.00039786 1/REarth

Two-line elements (TLE)

Creation date: July 8, 2025, 2:27 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 7, 2025, 9:53 p.m. UTC

TLE line 0: 0 ALOS DEB

TLE line 1: 1 36571U 06002AA 25188.91238284 .00003056 00000-0 39786-3 0 9991

TLE line 2: 2 36571 98.0003 154.8736 0000974 106.1028 254.0292 14.81356430812668

Live tracking on map

Real-time ground track for satellite ALOS DEB.

In-orbit conjunctions

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

Target Orbit TCA Probability of collision Miss distance Type
COSMOS 2251 DEB LEO 2024-11-19 12:16:00 0.0001258028 46.0 (m) DEBRIS

Associated space launch

ALOS (Advanced Land Observation Satellite) is used for cartography, regional observation, disaster monitoring, and resource surveying. ALOS has three remote-sensing instruments: - the Panchromatic Remote-sensing Instrument for Stereo Mapping (PRISM) for digital elevation mapping with 2.5 meter resolution, - the Advanced Visible and Near Infrared Radiometer type 2 (AVNIR-2) for precise land coverage observation with 10 meter resolution, and - the Phased Array type L-band Synthetic Aperture Radar (PALSAR) for day-and-night and all-weather land observation. ALOS transmitts its data via the DRTS (Kodama) satellite. The ALOS was launched by an H-2A-2022 launch vehicle from the Tanegashima Space Center. ALOS as been given the nickname Daichi. Five minutes after spacecraft separation, ALOS began to unfurl its 72-foot solar array that will provide electrical power to the craft throughout its mission. Six cameras are on-board to visually verify the correct deployment of the solar panel and various instrument antennas. ALOS lost all power on 22. April 2011, thus ending the mission.

ALOS DEB was lifted into orbit during the mission ‘H-IIA 2022 | Daichi’, on board a H-IIA 2022 space rocket.

The launch took place on Jan. 24, 2006, 1:33 a.m. from Yoshinobu Launch Complex LP-1.

For more information about the launch, click the button.

Launch to space H-IIA 2022 | Daichi
H-IIA 2022 | Daichi

Agency: N/A

Status: Launch Successful

Launch date: Jan. 24, 2006, 1:33 a.m. UTC

Rocket: H-IIA 2022

Launch pad: Yoshinobu Launch Complex LP-1

Location: Tanegashima Space Center, Japan

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