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 41918U 17003B 23152.53076265 .00000286 00000-0 94889-4 0 9999
2 41918 86.4008 192.9654 0002639 87.2874 272.8624 14.34220634333899
| Epoch (UTC): | 01 June 2023 12:44:17 |
| Eccentricity: | 0.0002639 |
| inclination: | 86.4008° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 192.9654° |
| argument of perigee: | 87.2874° |
| revolutions per day: | 14.34220634 |
| mean anomaly at epoch: | 272.8624° |
| orbit number at epoch: | 33389 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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