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 30208U 99025VR 24357.70872854 .00001991 00000-0 90863-3 0 9999
2 30208 98.5598 2.4977 0033738 221.4157 199.9763 14.22361785927881
| Epoch (UTC): | 22 December 2024 17:00:34 |
| Eccentricity: | 0.0033738 |
| inclination: | 98.5598° |
| perigee height: | 793 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 2.4977° |
| argument of perigee: | 221.4157° |
| revolutions per day: | 14.22361785 |
| mean anomaly at epoch: | 199.9763° |
| orbit number at epoch: | 92788 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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