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 20438U 90005C 23264.90368149 .00000152 00000-0 75204-4 0 9998
2 20438 98.9155 285.9876 0010450 37.6285 82.2672 14.31275700757255
| Epoch (UTC): | 21 September 2023 21:41:18 |
| Eccentricity: | 0.0010450 |
| inclination: | 98.9155° |
| perigee height: | 780 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 285.9876° |
| argument of perigee: | 37.6285° |
| revolutions per day: | 14.31275700 |
| mean anomaly at epoch: | 82.2672° |
| orbit number at epoch: | 75725 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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