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 44766C 19074BF 20057.86087274 .00002937 00000-0 20118-3 0 575
2 44766 53.0220 35.3710 0001621 56.3425 271.5805 15.05578174 17
| Epoch (UTC): | 26 February 2020 20:39:39 |
| Eccentricity: | 0.0001621 |
| inclination: | 53.0220° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 35.3710° |
| argument of perigee: | 56.3425° |
| revolutions per day: | 15.05578174 |
| mean anomaly at epoch: | 271.5805° |
| 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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