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 11U 59001A 24263.55726059 .00001466 00000-0 77857-3 0 9997
2 11 32.8682 328.1282 1454021 43.6337 327.0452 11.88736900801489
| Epoch (UTC): | 19 September 2024 13:22:27 |
| Eccentricity: | 0.1454021 |
| inclination: | 32.8682° |
| perigee height: | 552 km |
| apogee height: | 2911 km |
| right ascension of ascending node: | 328.1282° |
| argument of perigee: | 43.6337° |
| revolutions per day: | 11.88736900 |
| mean anomaly at epoch: | 327.0452° |
| orbit number at epoch: | 80148 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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