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 40057U 14034E 23336.85211570 .00006649 00000-0 81222-3 0 9997
2 40057 98.3580 177.6381 0010746 61.9133 298.3164 14.83603057508424
| Epoch (UTC): | 02 December 2023 20:27:02 |
| Eccentricity: | 0.0010746 |
| inclination: | 98.3580° |
| perigee height: | 610 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 177.6381° |
| argument of perigee: | 61.9133° |
| revolutions per day: | 14.83603057 |
| mean anomaly at epoch: | 298.3164° |
| orbit number at epoch: | 50842 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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