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 30899U 99025AYM 24352.41057104 .00009941 00000-0 39930-2 0 9991
2 30899 99.1958 223.4304 0032792 251.5783 282.6104 14.28069777915014
| Epoch (UTC): | 17 December 2024 09:51:13 |
| Eccentricity: | 0.0032792 |
| inclination: | 99.1958° |
| perigee height: | 774 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 223.4304° |
| argument of perigee: | 251.5783° |
| revolutions per day: | 14.28069777 |
| mean anomaly at epoch: | 282.6104° |
| orbit number at epoch: | 91501 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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