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 23025.94581443 .00003572 00000-0 43378-3 0 9990
2 00115 48.1664 10.7622 0033089 130.1779 230.2039 14.85230529333284
| Epoch (UTC): | 25 January 2023 22:41:58 |
| Eccentricity: | 0.0033089 |
| inclination: | 48.1664° |
| perigee height: | 590 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 10.7622° |
| argument of perigee: | 130.1779° |
| revolutions per day: | 14.85230529 |
| mean anomaly at epoch: | 230.2039° |
| orbit number at epoch: | 33328 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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