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 20625U 90046B 21025.88667082 .00000153 00000-0 10415-3 0 9992
2 20625 70.9984 261.3167 0016573 264.9126 95.0104 14.14666607584076
| Epoch (UTC): | 25 January 2021 21:16:48 |
| Eccentricity: | 0.0016573 |
| inclination: | 70.9984° |
| perigee height: | 831 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 261.3167° |
| argument of perigee: | 264.9126° |
| revolutions per day: | 14.14666607 |
| mean anomaly at epoch: | 95.0104° |
| orbit number at epoch: | 58407 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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