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 21024.73195112 -.00000067 00000-0 78924-5 0 9998
2 00116 66.8106 27.2630 0079550 217.9747 141.5708 13.91781927 22615
| Epoch (UTC): | 24 January 2021 17:34:00 |
| Eccentricity: | 0.0079550 |
| inclination: | 66.8106° |
| perigee height: | 864 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 27.2630° |
| argument of perigee: | 217.9747° |
| revolutions per day: | 13.91781927 |
| mean anomaly at epoch: | 141.5708° |
| orbit number at epoch: | 2261 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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