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 14781U 84021B 22178.56753710 .00000495 00000-0 66036-4 0 9993
2 14781 97.6173 165.5406 0006916 293.4111 66.6376 14.83692727 41543
| Epoch (UTC): | 27 June 2022 13:37:15 |
| Eccentricity: | 0.0006916 |
| inclination: | 97.6173° |
| perigee height: | 613 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 165.5406° |
| argument of perigee: | 293.4111° |
| revolutions per day: | 14.83692727 |
| mean anomaly at epoch: | 66.6376° |
| orbit number at epoch: | 4154 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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