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 24357.83165343 .00000169 00000-0 18715-3 0 9996
2 00116 66.8086 135.3408 0081413 290.9585 68.2796 13.92166833221345
| Epoch (UTC): | 22 December 2024 19:57:34 |
| Eccentricity: | 0.0081413 |
| inclination: | 66.8086° |
| perigee height: | 861 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 135.3408° |
| argument of perigee: | 290.9585° |
| revolutions per day: | 13.92166833 |
| mean anomaly at epoch: | 68.2796° |
| orbit number at epoch: | 22134 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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