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 41917U 17003A 23153.58997226 .00000317 00000-0 10602-3 0 9998
2 41917 86.4006 192.6199 0002256 85.6381 274.5072 14.34213732334020
| Epoch (UTC): | 02 June 2023 14:09:33 |
| Eccentricity: | 0.0002256 |
| inclination: | 86.4006° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 192.6199° |
| argument of perigee: | 85.6381° |
| revolutions per day: | 14.34213732 |
| mean anomaly at epoch: | 274.5072° |
| orbit number at epoch: | 33402 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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