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 27424U 02022A 21026.86446958 .00000094 00000-0 30924-4 0 9991
2 27424 98.2158 330.2318 0002076 47.8409 46.5739 14.57104459996403
| Epoch (UTC): | 26 January 2021 20:44:50 |
| Eccentricity: | 0.0002076 |
| inclination: | 98.2158° |
| perigee height: | 701 km |
| apogee height: | 704 km |
| right ascension of ascending node: | 330.2318° |
| argument of perigee: | 47.8409° |
| revolutions per day: | 14.57104459 |
| mean anomaly at epoch: | 46.5739° |
| orbit number at epoch: | 99640 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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