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 23341.33439390 .00026586 00000-0 14755-2 0 9990
2 39770 98.0011 115.1851 0004215 89.6956 270.4757 15.13717152518238
| Epoch (UTC): | 07 December 2023 08:01:31 |
| Eccentricity: | 0.0004215 |
| inclination: | 98.0011° |
| perigee height: | 522 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 115.1851° |
| argument of perigee: | 89.6956° |
| revolutions per day: | 15.13717152 |
| mean anomaly at epoch: | 270.4757° |
| orbit number at epoch: | 51823 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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