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 41922U 17003F 23153.56460804 .00000302 00000-0 10073-3 0 9995
2 41922 86.4009 192.5475 0002524 93.6268 266.5217 14.34215598334086
| Epoch (UTC): | 02 June 2023 13:33:02 |
| Eccentricity: | 0.0002524 |
| inclination: | 86.4009° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 192.5475° |
| argument of perigee: | 93.6268° |
| revolutions per day: | 14.34215598 |
| mean anomaly at epoch: | 266.5217° |
| orbit number at epoch: | 33408 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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