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 27432U 02024C 23154.61122689 .00000057 00000-0 53312-4 0 9996
2 27432 99.0234 189.0444 0050425 6.1294 105.0285 14.14214540 86455
| Epoch (UTC): | 03 June 2023 14:40:10 |
| Eccentricity: | 0.0050425 |
| inclination: | 99.0234° |
| perigee height: | 808 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 189.0444° |
| argument of perigee: | 6.1294° |
| revolutions per day: | 14.14214540 |
| mean anomaly at epoch: | 105.0285° |
| orbit number at epoch: | 8645 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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