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 42778U 17036P 23153.66264665 .00022143 00000-0 58892-3 0 9997
2 42778 97.1562 188.8551 0010126 144.2447 215.9478 15.38189229330495
| Epoch (UTC): | 02 June 2023 15:54:12 |
| Eccentricity: | 0.0010126 |
| inclination: | 97.1562° |
| perigee height: | 444 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 188.8551° |
| argument of perigee: | 144.2447° |
| revolutions per day: | 15.38189229 |
| mean anomaly at epoch: | 215.9478° |
| orbit number at epoch: | 33049 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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