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 25143.33923231 .00000026 00000-0 78683-4 0 9996
2 00116 66.8076 124.6817 0076306 191.8485 168.0803 13.92237125242436
| Epoch (UTC): | 23 May 2025 08:08:29 |
| Eccentricity: | 0.0076306 |
| inclination: | 66.8076° |
| perigee height: | 865 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 124.6817° |
| argument of perigee: | 191.8485° |
| revolutions per day: | 13.92237125 |
| mean anomaly at epoch: | 168.0803° |
| orbit number at epoch: | 24243 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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