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 27057U 01058C 21025.74176915 -.00000002 00000-0 -73016-4 0 9990
2 27057 82.5432 34.2850 0001000 117.6174 242.5028 12.61558225878640
| Epoch (UTC): | 25 January 2021 17:48:08 |
| Eccentricity: | 0.0001000 |
| inclination: | 82.5432° |
| perigee height: | 1416 km |
| apogee height: | 1417 km |
| right ascension of ascending node: | 34.2850° |
| argument of perigee: | 117.6174° |
| revolutions per day: | 12.61558225 |
| mean anomaly at epoch: | 242.5028° |
| orbit number at epoch: | 87864 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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