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 23038.79476901 .00003740 00000-0 45188-3 0 9997
2 115 48.1662 308.8151 0033737 187.2050 172.8382 14.85308458356357
Epoch (UTC): | 07 February 2023 19:04:28 |
Eccentricity: | 0.0033737 |
inclination: | 48.1662° |
perigee height: | 589 km |
apogee height: | 636 km |
right ascension of ascending node: | 308.8151° |
argument of perigee: | 187.2050° |
revolutions per day: | 14.85308458 |
mean anomaly at epoch: | 172.8382° |
orbit number at epoch: | 35635 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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