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 25136.37103442 .00000003 00000-0 61252-4 0 9995
2 00116 66.8072 141.7304 0076896 196.6291 163.2266 13.92235660241469
| Epoch (UTC): | 16 May 2025 08:54:17 |
| Eccentricity: | 0.0076896 |
| inclination: | 66.8072° |
| perigee height: | 864 km |
| apogee height: | 977 km |
| right ascension of ascending node: | 141.7304° |
| argument of perigee: | 196.6291° |
| revolutions per day: | 13.92235660 |
| mean anomaly at epoch: | 163.2266° |
| orbit number at epoch: | 24146 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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