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 39010U 12065C 22140.50119524 .00002995 00000-0 62336-3 0 9991
2 39010 49.6627 207.3340 4650004 326.2964 11.3772 6.18338467212595
| Epoch (UTC): | 20 May 2022 12:01:43 |
| Eccentricity: | 0.4650004 |
| inclination: | 49.6627° |
| perigee height: | 330 km |
| apogee height: | 11991 km |
| right ascension of ascending node: | 207.3340° |
| argument of perigee: | 326.2964° |
| revolutions per day: | 6.18338467 |
| mean anomaly at epoch: | 11.3772° |
| orbit number at epoch: | 21259 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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