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 04394U 70037B 23032.51615411 .00010815 00000-0 28865-3 0 9998
2 04394 81.2394 112.6995 0031865 279.9200 79.8444 15.37455824879604
| Epoch (UTC): | 01 February 2023 12:23:15 |
| Eccentricity: | 0.0031865 |
| inclination: | 81.2394° |
| perigee height: | 432 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 112.6995° |
| argument of perigee: | 279.9200° |
| revolutions per day: | 15.37455824 |
| mean anomaly at epoch: | 79.8444° |
| orbit number at epoch: | 87960 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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