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 22023.93405164 .00007613 00000-0 24253-3 0 9999
2 39026 97.2610 16.8955 0032242 320.2679 39.6202 15.32320364506768
| Epoch (UTC): | 23 January 2022 22:25:02 |
| Eccentricity: | 0.0032242 |
| inclination: | 97.2610° |
| perigee height: | 447 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 16.8955° |
| argument of perigee: | 320.2679° |
| revolutions per day: | 15.32320364 |
| mean anomaly at epoch: | 39.6202° |
| orbit number at epoch: | 50676 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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