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 25137.73593965 .00000028 00000-0 79966-4 0 9997
2 00116 66.8072 138.3909 0076774 195.6952 164.1748 13.92236058241658
| Epoch (UTC): | 17 May 2025 17:39:45 |
| Eccentricity: | 0.0076774 |
| inclination: | 66.8072° |
| perigee height: | 865 km |
| apogee height: | 977 km |
| right ascension of ascending node: | 138.3909° |
| argument of perigee: | 195.6952° |
| revolutions per day: | 13.92236058 |
| mean anomaly at epoch: | 164.1748° |
| orbit number at epoch: | 24165 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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