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 10820U 78042A 23159.53294558 .00000494 00000-0 18485-3 0 9999
2 10820 98.4957 355.3842 0010410 47.1841 313.0218 14.35986155354351
| Epoch (UTC): | 08 June 2023 12:47:26 |
| Eccentricity: | 0.0010410 |
| inclination: | 98.4957° |
| perigee height: | 764 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 355.3842° |
| argument of perigee: | 47.1841° |
| revolutions per day: | 14.35986155 |
| mean anomaly at epoch: | 313.0218° |
| orbit number at epoch: | 35435 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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