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 41465U 16026B 22178.95779030 .00010074 00000-0 24006-3 0 9992
2 41465 97.0559 54.9512 0011600 93.0163 322.1864 15.41699570345154
| Epoch (UTC): | 27 June 2022 22:59:13 |
| Eccentricity: | 0.0011600 |
| inclination: | 97.0559° |
| perigee height: | 433 km |
| apogee height: | 449 km |
| right ascension of ascending node: | 54.9512° |
| argument of perigee: | 93.0163° |
| revolutions per day: | 15.41699570 |
| mean anomaly at epoch: | 322.1864° |
| orbit number at epoch: | 34515 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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