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 38758U 12048A 23075.71345785 0.00000000 00000-0 00000-0 0 06
2 38758 63.4302 359.0622 0212121 358.9114 1.0886 13.40727588 06
| Epoch (UTC): | 16 March 2023 17:07:22 |
| Eccentricity: | 0.0212121 |
| inclination: | 63.4302° |
| perigee height: | 948 km |
| apogee height: | 1265 km |
| right ascension of ascending node: | 359.0622° |
| argument of perigee: | 358.9114° |
| revolutions per day: | 13.40727588 |
| mean anomaly at epoch: | 1.0886° |
| 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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