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 23344.14889281 .00002007 00000-0 24085-3 0 9993
2 00115 48.1643 273.6186 0031997 99.8115 260.6414 14.87729354380622
Epoch (UTC): | 10 December 2023 03:34:24 |
Eccentricity: | 0.0031997 |
inclination: | 48.1643° |
perigee height: | 582 km |
apogee height: | 627 km |
right ascension of ascending node: | 273.6186° |
argument of perigee: | 99.8115° |
revolutions per day: | 14.87729354 |
mean anomaly at epoch: | 260.6414° |
orbit number at epoch: | 38062 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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