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 23150.34472613 .00018493 00000-0 49488-3 0 9997
2 42778 97.1571 185.6188 0009827 153.8095 206.3650 15.38037416329985
| Epoch (UTC): | 30 May 2023 08:16:24 |
| Eccentricity: | 0.0009827 |
| inclination: | 97.1571° |
| perigee height: | 445 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 185.6188° |
| argument of perigee: | 153.8095° |
| revolutions per day: | 15.38037416 |
| mean anomaly at epoch: | 206.3650° |
| orbit number at epoch: | 32998 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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