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 39770U 14029E 23080.12755118 .00026345 00000-0 22280-2 0 9991
2 39770 97.9577 205.1637 0008937 247.5004 112.4192 14.97992518478953
| Epoch (UTC): | 21 March 2023 03:03:40 |
| Eccentricity: | 0.0008937 |
| inclination: | 97.9577° |
| perigee height: | 567 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 205.1637° |
| argument of perigee: | 247.5004° |
| revolutions per day: | 14.97992518 |
| mean anomaly at epoch: | 112.4192° |
| orbit number at epoch: | 47895 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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