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 41607U 16040J 23083.66452191 .00131519 00000-0 22745-2 0 9991
2 41607 97.1684 133.9015 0008625 179.6240 180.5020 15.50443849375843
| Epoch (UTC): | 24 March 2023 15:56:54 |
| Eccentricity: | 0.0008625 |
| inclination: | 97.1684° |
| perigee height: | 409 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 133.9015° |
| argument of perigee: | 179.6240° |
| revolutions per day: | 15.50443849 |
| mean anomaly at epoch: | 180.5020° |
| orbit number at epoch: | 37584 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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