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MATS, 54227

Orbit data source: Space-Track

MATS, 54227 is a payload satellite owned by SNSB (SE) in SSO that was launched on Fri, 04 Nov 2022 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
54227, 2022-147A
Orbit
SSO
Last TLE update
11 hours ago
Origin
Manufacturer
OHB-SE
Mission
Operational Civil Science
Bus & Motor
INNOSAT, Unknown motor
Mass
54 kg wet, 54 kg dry
Launch date (UTC)
2022-11-04 (3 years ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.8 m
Radar Cross Section
0.660 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 11 hours ago
0 MATS
1 54227U 22147A   25128.91053477  .00004026  00000-0  31146-3 0  9990
2 54227  97.6728 128.6171 0017226 120.7533 239.5390 15.01928196137011
Epoch: 2025-05-08T21:51Z
Definitive object data (Epoch: 2025-05-08T21:51:10.204Z)
Latitude
-0.00006°
Longitude
-66.14966°
Altitude
570.085 km
Speed
7.573 km/s
True Right ascension
08h 34m 28s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at TLE epoch
Visualization TLE readout
Latitude
-19.10148°
Longitude
-63.0325°
Altitude
577.281 km
Speed
7.566 km/s
Apparent Right ascension
07h 14m 17s
Apparent Declination
-31° 49' 29"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
17:06:51
Azimuth
277.445° WNW
Elevation
-63.108°
Doppler factor
1
Orbital elements
Apogee altitude
569.901 km
Perigee altitude
546.004 km
Semi-major axis
6,936.089 km
Eccentricity
0.0017226
Inclination
97.6728°
RAAN
128.6171°
Arg. of periapsis
120.7533°
True anomaly
239.36904°
Mean anomaly
239.539°
Eccentric anomaly
239.454°
Mean motion
3.75726 °/min
BSTAR
0.00031146
Orbital period
95.81 mins
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Other satellites on launch #147 in the year 2022 (2022-11-04 UTC)

MATS Visibility forecast

Observer location: undefined°, undefined°

Span
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Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
7 mins2025-05-09 12:48:36.367Z13.173° NNE2025-05-09 12:51:36.367Z37.289° NE44.814°2025-05-09 12:55:36.367Z192.418° SSW
6 mins2025-05-09 23:34:36.367Z138.472° SSE2025-05-09 23:37:36.367Z54.07° ENE34.17°2025-05-09 23:40:36.367Z2.705° NNE
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