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 23152.82251316 .00000301 00000-0 10031-3 0 9996
2 41917 86.4008 192.9402 0002280 83.1952 276.9503 14.34223023333912
| Epoch (UTC): | 01 June 2023 19:44:25 |
| Eccentricity: | 0.0002280 |
| inclination: | 86.4008° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 192.9402° |
| argument of perigee: | 83.1952° |
| revolutions per day: | 14.34223023 |
| mean anomaly at epoch: | 276.9503° |
| orbit number at epoch: | 33391 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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