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 59099U 24043B 24280.58519584 .00019693 00000-0 17801-2 0 9993
2 59099 97.7731 42.7269 0009245 283.3660 76.6529 14.95453964 32185
| Epoch (UTC): | 06 October 2024 14:02:40 |
| Eccentricity: | 0.0009245 |
| inclination: | 97.7731° |
| perigee height: | 574 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 42.7269° |
| argument of perigee: | 283.3660° |
| revolutions per day: | 14.95453964 |
| mean anomaly at epoch: | 76.6529° |
| orbit number at epoch: | 3218 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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