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 38773U 12048P 23075.71337515 0.00000000 00000-0 00000-0 0 05
2 38773 63.4308 358.8653 0213356 358.8613 1.1387 13.40727647 07
| Epoch (UTC): | 16 March 2023 17:07:15 |
| Eccentricity: | 0.0213356 |
| inclination: | 63.4308° |
| perigee height: | 947 km |
| apogee height: | 1266 km |
| right ascension of ascending node: | 358.8653° |
| argument of perigee: | 358.8613° |
| revolutions per day: | 13.40727647 |
| mean anomaly at epoch: | 1.1387° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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