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 44718C 19074F 21025.24981927 .00008429 00000-0 56487-3 0 253
2 44718 53.0553 298.8424 0001934 75.5042 53.6818 15.06384022 17
| Epoch (UTC): | 25 January 2021 05:59:44 |
| Eccentricity: | 0.0001934 |
| inclination: | 53.0553° |
| perigee height: | 546 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 298.8424° |
| argument of perigee: | 75.5042° |
| revolutions per day: | 15.06384022 |
| mean anomaly at epoch: | 53.6818° |
| 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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