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 00116U 61015A 21059.65614547 -.00000038 00000-0 29676-4 0 9992
2 00116 66.8100 301.8866 0076826 194.3292 165.5609 13.91784474 27472
| Epoch (UTC): | 28 February 2021 15:44:50 |
| Eccentricity: | 0.0076826 |
| inclination: | 66.8100° |
| perigee height: | 866 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 301.8866° |
| argument of perigee: | 194.3292° |
| revolutions per day: | 13.91784474 |
| mean anomaly at epoch: | 165.5609° |
| orbit number at epoch: | 2747 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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