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 45409C 20019BB 21020.19013306 .00013292 00000-0 90958-3 0 208
2 45409 52.9990 271.5786 0001867 73.5114 61.4051 15.05600242 10
| Epoch (UTC): | 20 January 2021 04:33:47 |
| Eccentricity: | 0.0001867 |
| inclination: | 52.9990° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 271.5786° |
| argument of perigee: | 73.5114° |
| revolutions per day: | 15.05600242 |
| mean anomaly at epoch: | 61.4051° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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