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 39026U 12072A 22022.49738374 .00008535 00000-0 27171-3 0 9997
2 39026 97.2606 15.4865 0032418 325.5741 34.3400 15.32298389506540
| Epoch (UTC): | 22 January 2022 11:56:13 |
| Eccentricity: | 0.0032418 |
| inclination: | 97.2606° |
| perigee height: | 447 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 15.4865° |
| argument of perigee: | 325.5741° |
| revolutions per day: | 15.32298389 |
| mean anomaly at epoch: | 34.3400° |
| orbit number at epoch: | 50654 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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