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 30688U 99025AQW 24355.73321029 .00006636 00000-0 26661-2 0 9990
2 30688 98.7230 62.4507 0017047 280.9682 205.6768 14.28392152922110
| Epoch (UTC): | 20 December 2024 17:35:49 |
| Eccentricity: | 0.0017047 |
| inclination: | 98.7230° |
| perigee height: | 785 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 62.4507° |
| argument of perigee: | 280.9682° |
| revolutions per day: | 14.28392152 |
| mean anomaly at epoch: | 205.6768° |
| orbit number at epoch: | 92211 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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