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 41460U 16025E 23083.55584032 .00088536 00000-0 19074-2 0 9990
2 41460 98.1702 286.5835 0082152 354.9431 63.2962 15.40691119380677
| Epoch (UTC): | 24 March 2023 13:20:24 |
| Eccentricity: | 0.0082152 |
| inclination: | 98.1702° |
| perigee height: | 388 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 286.5835° |
| argument of perigee: | 354.9431° |
| revolutions per day: | 15.40691119 |
| mean anomaly at epoch: | 63.2962° |
| orbit number at epoch: | 38067 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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