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 30892U 99025AYE 24245.45440537 .00002551 00000-0 12736-2 0 9990
2 30892 99.6509 142.1462 0040521 53.7730 306.7177 14.17438501576798
| Epoch (UTC): | 01 September 2024 10:54:20 |
| Eccentricity: | 0.0040521 |
| inclination: | 99.6509° |
| perigee height: | 805 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 142.1462° |
| argument of perigee: | 53.7730° |
| revolutions per day: | 14.17438501 |
| mean anomaly at epoch: | 306.7177° |
| orbit number at epoch: | 57679 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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