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 27844U 03031E 21015.74971788 .00000040 00000-0 37740-4 0 9991
2 27844 98.6815 26.2695 0010282 155.6596 204.5070 14.22282190910272
| Epoch (UTC): | 15 January 2021 17:59:35 |
| Eccentricity: | 0.0010282 |
| inclination: | 98.6815° |
| perigee height: | 810 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 26.2695° |
| argument of perigee: | 155.6596° |
| revolutions per day: | 14.22282190 |
| mean anomaly at epoch: | 204.5070° |
| orbit number at epoch: | 91027 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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