View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 39134U 13015E 23087.57851788 .00090147 00000-0 17133-2 0 9997
2 39134 64.8536 200.7152 0019073 258.3000 101.6001 15.47557288550459
Epoch (UTC): | 28 March 2023 13:53:03 |
Eccentricity: | 0.0019073 |
inclination: | 64.8536° |
perigee height: | 411 km |
apogee height: | 437 km |
right ascension of ascending node: | 200.7152° |
argument of perigee: | 258.3000° |
revolutions per day: | 15.47557288 |
mean anomaly at epoch: | 101.6001° |
orbit number at epoch: | 55045 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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