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 115U 60002D 22147.26084166 .00001329 00000-0 18167-3 0 9995
2 115 48.1645 104.6195 0033488 134.2677 226.0992 14.84352269318230
Epoch (UTC): | 27 May 2022 06:15:36 |
Eccentricity: | 0.0033488 |
inclination: | 48.1645° |
perigee height: | 592 km |
apogee height: | 639 km |
right ascension of ascending node: | 104.6195° |
argument of perigee: | 134.2677° |
revolutions per day: | 14.84352269 |
mean anomaly at epoch: | 226.0992° |
orbit number at epoch: | 31823 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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