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 00029U 60002B 21020.87461398 -.00000118 00000-0 13486-4 0 9997
2 00029 48.3808 2.5108 0023396 82.3310 278.0257 14.74398957250623
| Epoch (UTC): | 20 January 2021 20:59:26 |
| Eccentricity: | 0.0023396 |
| inclination: | 48.3808° |
| perigee height: | 630 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 2.5108° |
| argument of perigee: | 82.3310° |
| revolutions per day: | 14.74398957 |
| mean anomaly at epoch: | 278.0257° |
| orbit number at epoch: | 25062 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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