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 116U 61015A 25140.25023823 .00000028 00000-0 79651-4 0 9990
2 116 66.8072 132.2393 0076571 193.9771 165.9191 13.92236488242506
| Epoch (UTC): | 20 May 2025 06:00:20 |
| Eccentricity: | 0.0076571 |
| inclination: | 66.8072° |
| perigee height: | 865 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 132.2393° |
| argument of perigee: | 193.9771° |
| revolutions per day: | 13.92236488 |
| mean anomaly at epoch: | 165.9191° |
| orbit number at epoch: | 24250 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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