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 65960U 26145.43432010 +.00000000 +00000-0 +93278-3 0 00006
2 65960 51.8735 307.9636 0005142 218.8300 141.2319 15.40655291 04
| Epoch (UTC): | 25 May 2026 10:25:25 |
| Eccentricity: | 0.0005142 |
| inclination: | 51.8735° |
| perigee height: | 441 km |
| apogee height: | 448 km |
| right ascension of ascending node: | 307.9636° |
| argument of perigee: | 218.8300° |
| revolutions per day: | 15.40655291 |
| mean anomaly at epoch: | 141.2319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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