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 00115U 60002D 22148.27054474 .00001384 00000-0 18806-3 0 9997
2 00115 48.1663 99.7587 0033558 138.5742 221.7724 14.84355519297228
Epoch (UTC): | 28 May 2022 06:29:35 |
Eccentricity: | 0.0033558 |
inclination: | 48.1663° |
perigee height: | 592 km |
apogee height: | 639 km |
right ascension of ascending node: | 99.7587° |
argument of perigee: | 138.5742° |
revolutions per day: | 14.84355519 |
mean anomaly at epoch: | 221.7724° |
orbit number at epoch: | 29722 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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