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 21021.85624918 .00000257 00000-0 15828-3 0 9994
2 20625 70.9988 269.7767 0016477 269.9860 89.9374 14.14664537583509
| Epoch (UTC): | 21 January 2021 20:32:59 |
| Eccentricity: | 0.0016477 |
| inclination: | 70.9988° |
| perigee height: | 831 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 269.7767° |
| argument of perigee: | 269.9860° |
| revolutions per day: | 14.14664537 |
| mean anomaly at epoch: | 89.9374° |
| orbit number at epoch: | 58350 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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