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 04190U 69082BD 23341.39711198 .00010758 00000-0 98516-3 0 9994
2 04190 70.0243 51.8854 0024848 352.8832 7.1969 14.94915089852760
| Epoch (UTC): | 07 December 2023 09:31:50 |
| Eccentricity: | 0.0024848 |
| inclination: | 70.0243° |
| perigee height: | 565 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 51.8854° |
| argument of perigee: | 352.8832° |
| revolutions per day: | 14.94915089 |
| mean anomaly at epoch: | 7.1969° |
| orbit number at epoch: | 85276 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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