ALOS

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite ALOS at a glance.

Uptime

7044

Days in orbit

Revolutions

≈ 14.7

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.1

Latest

Satellite identification and parameters

Extended collection of information and parameters for ALOS.

Object identification

Identified? True

Debris? False

Object name: ALOS

International designator: 2006-002A

Object number (NORAD): 28931

Object ID (CCSDS): 28931

Country: JAPAN (JPN)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 98.052 minutes

Inclination: 98.0814 deg

SMA: 7043.674 km

Apoapsis: 666.75 km

Periapsis: 664.327 km

RAAN: 81.5263 deg

Eccentricy: 0.000172

Argument of periapsis: 113.5708 deg

Mean anomaly: 246.5678 deg

Mean motion: 14.68601335 rev/day

Mean motion (dot): 0.00001943 rev/day2

B* drag term: 0.00034279 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, 9:50 p.m. UTC

TLE line 0: 0 ALOS

TLE line 1: 1 28931U 06002A 25127.91004478 .00001943 00000-0 34279-3 0 9996

TLE line 2: 2 28931 98.0814 81.5263 0001720 113.5708 246.5678 14.68601335 28583

Live tracking on map

Real-time ground track for satellite ALOS.

In-orbit conjunctions

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

Target Orbit TCA Probability of collision Miss distance Type
IRIDIUM 33 DEB LEO 2024-11-30 18:11:29 0.0001081432 765.0 (m) DEBRIS
CZ-6A DEB LEO 2024-10-31 10:38:37 0.0005921226 576.0 (m) DEBRIS
CZ-4B DEB LEO 2024-10-28 14:07:41 0.0002472595 283.0 (m) DEBRIS
DMSP 5D-2 F13 DEB SSO 2024-06-09 08:31:39 0.0002375124 68.0 (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 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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