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 23339.81395990 .00037924 00000-0 21053-2 0 9994
2 39770 98.0010 113.5881 0004409 97.5636 262.6094 15.13621612518007
| Epoch (UTC): | 05 December 2023 19:32:06 |
| Eccentricity: | 0.0004409 |
| inclination: | 98.0010° |
| perigee height: | 522 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 113.5881° |
| argument of perigee: | 97.5636° |
| revolutions per day: | 15.13621612 |
| mean anomaly at epoch: | 262.6094° |
| orbit number at epoch: | 51800 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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