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 is defined by the following mean orbital elements,
1 65432U 25193A 25274.36939949 0.00073149 00000-0 30749-2 0 04
2 65432 139.3541 156.1753 0165002 271.9256 87.5625 15.10966676 02
| Epoch (UTC): | 01 October 2025 08:51:56 |
| Eccentricity: | 0.0165002 |
| inclination: | 139.3541° |
| perigee height: | 419 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 156.1753° |
| argument of perigee: | 271.9256° |
| revolutions per day: | 15.10966676 |
| mean anomaly at epoch: | 87.5625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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