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 23156.73296451 .00000047 00000-0 48059-4 0 9991
2 27432 99.0233 191.1875 0050314 0.1378 107.1564 14.14214893 86836
| Epoch (UTC): | 05 June 2023 17:35:28 |
| Eccentricity: | 0.0050314 |
| inclination: | 99.0233° |
| perigee height: | 808 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 191.1875° |
| argument of perigee: | 0.1378° |
| revolutions per day: | 14.14214893 |
| mean anomaly at epoch: | 107.1564° |
| orbit number at epoch: | 8683 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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