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 23336.90499240 .00035081 00000-0 19609-2 0 9990
2 39770 98.0018 110.5352 0004548 107.6464 252.5262 15.13394424517564
| Epoch (UTC): | 02 December 2023 21:43:11 |
| Eccentricity: | 0.0004548 |
| inclination: | 98.0018° |
| perigee height: | 523 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 110.5352° |
| argument of perigee: | 107.6464° |
| revolutions per day: | 15.13394424 |
| mean anomaly at epoch: | 252.5262° |
| orbit number at epoch: | 51756 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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