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 23153.61992427 .00000065 00000-0 57450-4 0 9996
2 27432 99.0234 188.0431 0050465 8.9223 98.1455 14.14214433 86313
| Epoch (UTC): | 02 June 2023 14:52:41 |
| Eccentricity: | 0.0050465 |
| inclination: | 99.0234° |
| perigee height: | 808 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 188.0431° |
| argument of perigee: | 8.9223° |
| revolutions per day: | 14.14214433 |
| mean anomaly at epoch: | 98.1455° |
| orbit number at epoch: | 8631 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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