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 25141.39963155 .00000030 00000-0 81131-4 0 9996
2 00116 66.8073 129.4272 0076466 193.1839 166.7244 13.92236707242165
| Epoch (UTC): | 21 May 2025 09:35:28 |
| Eccentricity: | 0.0076466 |
| inclination: | 66.8073° |
| perigee height: | 865 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 129.4272° |
| argument of perigee: | 193.1839° |
| revolutions per day: | 13.92236707 |
| mean anomaly at epoch: | 166.7244° |
| orbit number at epoch: | 24216 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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