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 23151.82673810 .00000280 00000-0 92980-4 0 9999
2 41923 86.4009 193.2602 0002062 91.5031 268.6401 14.34219237333811
| Epoch (UTC): | 31 May 2023 19:50:30 |
| Eccentricity: | 0.0002062 |
| inclination: | 86.4009° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 193.2602° |
| argument of perigee: | 91.5031° |
| revolutions per day: | 14.34219237 |
| mean anomaly at epoch: | 268.6401° |
| orbit number at epoch: | 33381 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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