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 22626U 93024A 21015.71282790 .00000193 00000-0 18137-4 0 9998
2 22626 82.5209 247.7778 0020379 95.6228 264.7315 14.88071126500721
| Epoch (UTC): | 15 January 2021 17:06:28 |
| Eccentricity: | 0.0020379 |
| inclination: | 82.5209° |
| perigee height: | 590 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 247.7778° |
| argument of perigee: | 95.6228° |
| revolutions per day: | 14.88071126 |
| mean anomaly at epoch: | 264.7315° |
| orbit number at epoch: | 50072 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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