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 41603U 16040E 22274.89434352 .00001556 00000-0 73148-4 0 9994
2 41603 97.1977 307.2520 0014244 141.1204 301.6460 15.20924816348219
| Epoch (UTC): | 01 October 2022 21:27:51 |
| Eccentricity: | 0.0014244 |
| inclination: | 97.1977° |
| perigee height: | 493 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 307.2520° |
| argument of perigee: | 141.1204° |
| revolutions per day: | 15.20924816 |
| mean anomaly at epoch: | 301.6460° |
| orbit number at epoch: | 34821 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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