DECAYED

H-2A R/B, 45166 (Decayed)

Orbit data source: Space-Track

H-2A R/B, 45166 was space debris in LEO originally from a launch on Sun, 09 Feb 2020 UTC launched from the Tanegashima Space Center (TNSTA). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

Not visible in the next 10 days

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/45166?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/45166?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

Max 10 NORAD IDs; Separated by commas

Initial load time (optional)

ISO8601 Format

TLE date request (optional)

ISO8601 Format

Identifier

45166, 2020-009B

Orbit

Decayed

Last TLE update

1 year ago

Origin

Mitsubishi Heavy Industries (MHI) (JP / JPN)

Manufacturer

MHI Tobishima

Mission

Decayed spacecraft

Bus & Motor

H-2A STAGE 2, Unknown motor

Mass

4,000 kg wet, 4,000 kg dry

Launch date (UTC)

2020-02-09 (5 years ago)

Launch vehicle

Unknown

Launch site

Tanegashima Space Center (TNSTA)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 9.2 m

Radar Cross Section

35.186 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 year ago

0 H-2A R/B
1 45166U 20009B   24113.86650667  .53867009  26681-5  20022-3 0  9993
2 45166  96.9487 155.0121 0009591 232.7556 210.3324 16.58268437235483

Epoch: 2024-04-22T20:47Z

TLE epoch observation values (Epoch: 2024-04-22T20:47:46.176Z)

Latitude

80.2214°

Longitude

-53.0038°

Altitude

136.426 km

Speed

7.828 km/s

True Right ascension

07h 21m 21s

True Declination

80° 09' 29"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

120.644 km

Perigee altitude

108.19 km

Semi-major axis

6,492.554 km

Eccentricity

0.00096

Inclination

96.9487°

RAAN

155.0121°

Arg. of periapsis

232.7556°

True anomaly

Unknown

Mean anomaly

210.3324°

Eccentric anomaly

Unknown

Mean motion

4.14877 °/min

Orbital period

86.77 mins

BSTAR

0.00020022

Loading maneuver chart data...

Loading SW <> Apogee altitude chart data...

Loading historical data...

Other satellites on launch #9 in the year 2020 (2020-02-09 UTC)

IGS O-7, 45165

H-2A R/B Visibility

Observer location: undefined°, undefined°

This satellite is decayed

Authenticating...

Click to sort rows by Secondary header in ascending order	Click to sort rows by Secondary name header in ascending order	Click to sort rows by Country header in ascending order	Click to sort rows by Owner header in ascending order	Click to sort rows by Obj. Type header in ascending order	Click to sort rows by Miss dist. header in ascending order	Click to sort rows by Rel. speed header in ascending order	Click to sort rows by Apr. angle header in ascending order	Click to sort rows by TCA header in ascending order

Check out H-2A R/B, 45166 (Decayed) on other resources

View H-2A R/B, 45166 (Decayed) on Celestrak

View H-2A R/B, 45166 (Decayed) on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.