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 23027.29128661 .00002842 00000-0 35049-3 0 9994
2 00115 48.1666 4.2761 0033126 136.1927 224.1622 14.85237975333485
| Epoch (UTC): | 27 January 2023 06:59:27 |
| Eccentricity: | 0.0033126 |
| inclination: | 48.1666° |
| perigee height: | 589 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 4.2761° |
| argument of perigee: | 136.1927° |
| revolutions per day: | 14.85237975 |
| mean anomaly at epoch: | 224.1622° |
| orbit number at epoch: | 33348 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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