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 30120U 99025RZ 23335.91022684 .00008707 00000-0 41486-2 0 9996
2 30120 98.8992 41.2763 0073518 188.4481 282.4576 14.18100406868218
| Epoch (UTC): | 01 December 2023 21:50:43 |
| Eccentricity: | 0.0073518 |
| inclination: | 98.8992° |
| perigee height: | 779 km |
| apogee height: | 885 km |
| right ascension of ascending node: | 41.2763° |
| argument of perigee: | 188.4481° |
| revolutions per day: | 14.18100406 |
| mean anomaly at epoch: | 282.4576° |
| orbit number at epoch: | 86821 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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