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 23335.91318726 .00065031 00000-0 36299-2 0 9991
2 39770 98.0020 109.4945 0004482 111.7235 248.4472 15.13263246517419
| Epoch (UTC): | 01 December 2023 21:54:59 |
| Eccentricity: | 0.0004482 |
| inclination: | 98.0020° |
| perigee height: | 523 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 109.4945° |
| argument of perigee: | 111.7235° |
| revolutions per day: | 15.13263246 |
| mean anomaly at epoch: | 248.4472° |
| orbit number at epoch: | 51741 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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