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 41923U 17003G 23159.50127197 .00000305 00000-0 10169-3 0 9990
2 41923 86.4002 190.0575 0002073 93.6831 266.4601 14.34219893334919
| Epoch (UTC): | 08 June 2023 12:01:49 |
| Eccentricity: | 0.0002073 |
| inclination: | 86.4002° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 190.0575° |
| argument of perigee: | 93.6831° |
| revolutions per day: | 14.34219893 |
| mean anomaly at epoch: | 266.4601° |
| orbit number at epoch: | 33491 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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