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 24250.43527438 .00009910 00000-0 10113-2 0 9991
2 00115 48.1636 37.8073 0031572 226.9047 132.9225 14.90690916421054
| Epoch (UTC): | 06 September 2024 10:26:47 |
| Eccentricity: | 0.0031572 |
| inclination: | 48.1636° |
| perigee height: | 574 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 37.8073° |
| argument of perigee: | 226.9047° |
| revolutions per day: | 14.90690916 |
| mean anomaly at epoch: | 132.9225° |
| orbit number at epoch: | 42105 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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