SOHLA-1 (MAIDO-1)

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite SOHLA-1 (MAIDO-1) at a glance.

Uptime

6008

Days in orbit

Revolutions

≈ 14.7

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.2

Latest

Satellite identification and parameters

Extended collection of information and parameters for SOHLA-1 (MAIDO-1).

Object identification

Identified? True

Debris? False

Object name: SOHLA-1 (MAIDO-1)

International designator: 2009-002E

Object number (NORAD): 33496

Object ID (CCSDS): 33496

Country: JAPAN (JPN)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 97.662 minutes

Inclination: 98.1666 deg

SMA: 7024.943 km

Apoapsis: 651.699 km

Periapsis: 641.916 km

RAAN: 83.7714 deg

Eccentricy: 0.0006963

Argument of periapsis: 52.1662 deg

Mean anomaly: 308.0175 deg

Mean motion: 14.74478982 rev/day

Mean motion (dot): 0.00000408 rev/day2

B* drag term: 0.00006926 1/REarth

Two-line elements (TLE)

Creation date: July 5, 2025, 5:45 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 5, 2025, 7:31 a.m. UTC

TLE line 0: 0 SOHLA-1 (MAIDO-1)

TLE line 1: 1 33496U 09002E 25186.31365594 .00000408 00000-0 69260-4 0 9993

TLE line 2: 2 33496 98.1666 83.7714 0006963 52.1662 308.0175 14.74478982882869

Live tracking on map

Real-time ground track for satellite SOHLA-1 (MAIDO-1).

In-orbit conjunctions

A list of the most updated potential collisions computed for object SOHLA-1 (MAIDO-1).

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB SSO 2025-05-19 16:54:45 0.0002764809 904.0 (m) DEBRIS
CZ-4C R/B SSO 2024-10-27 17:34:25 0.0001522884 156.0 (m) ROCKET BODY
CZ-6A DEB SSO 2024-09-30 23:54:17 0.0001015603 199.0 (m) DEBRIS

Associated space launch

Japanese Earth observation satellite. Launched with 7 secondary payloads.

SOHLA-1 (MAIDO-1) was lifted into orbit during the mission ‘H-IIA 202 | GOSAT’, on board a H-IIA space rocket.

The launch took place on Jan. 23, 2009, 3:54 a.m. from Yoshinobu Launch Complex LP-1.

For more information about the launch, click the button.

Launch to space H-IIA 202 | GOSAT
H-IIA 202 | GOSAT

Agency: N/A

Status: Launch Successful

Launch date: Jan. 23, 2009, 3:54 a.m. UTC

Rocket: H-IIA

Launch pad: Yoshinobu Launch Complex LP-1

Location: Tanegashima Space Center, Japan

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