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 00965U 64083D 25347.85857351 .00000097 00000-0 12147-3 0 9998
2 00965 90.0672 201.6067 0043376 99.4445 271.9936 13.56991088 18484
| Epoch (UTC): | 13 December 2025 20:36:20 |
| Eccentricity: | 0.0043376 |
| inclination: | 90.0672° |
| perigee height: | 1014 km |
| apogee height: | 1079 km |
| right ascension of ascending node: | 201.6067° |
| argument of perigee: | 99.4445° |
| revolutions per day: | 13.56991088 |
| mean anomaly at epoch: | 271.9936° |
| orbit number at epoch: | 1848 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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