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 00053U 60009E 21059.81443453 -.00000017 00000-0 66958-3 0 9998
2 00053 47.2745 188.4093 0099990 119.3612 241.7206 12.17254826699791
| Epoch (UTC): | 28 February 2021 19:32:47 |
| Eccentricity: | 0.0099990 |
| inclination: | 47.2745° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 188.4093° |
| argument of perigee: | 119.3612° |
| revolutions per day: | 12.17254826 |
| mean anomaly at epoch: | 241.7206° |
| orbit number at epoch: | 69979 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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