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 23028.90584089 .00002395 00000-0 29951-3 0 9991
2 00115 48.1662 356.4917 0033221 143.4351 216.8839 14.85248065333721
Epoch (UTC): | 28 January 2023 21:44:24 |
Eccentricity: | 0.0033221 |
inclination: | 48.1662° |
perigee height: | 589 km |
apogee height: | 636 km |
right ascension of ascending node: | 356.4917° |
argument of perigee: | 143.4351° |
revolutions per day: | 14.85248065 |
mean anomaly at epoch: | 216.8839° |
orbit number at epoch: | 33372 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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