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 16263U 85108B 25348.81317130 .00000663 00000-0 74020-4 0 9998
2 16263 82.5033 81.0265 0018747 196.7153 285.7939 14.85407076143320
| Epoch (UTC): | 14 December 2025 19:30:58 |
| Eccentricity: | 0.0018747 |
| inclination: | 82.5033° |
| perigee height: | 599 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 81.0265° |
| argument of perigee: | 196.7153° |
| revolutions per day: | 14.85407076 |
| mean anomaly at epoch: | 285.7939° |
| orbit number at epoch: | 14332 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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