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 65042U 26145.58335647 +.00000000 +00000-0 -55940-3 0 00006
2 65042 53.1594 296.7862 0001581 91.8277 356.5919 15.33555663 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001581 |
| inclination: | 53.1594° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 296.7862° |
| argument of perigee: | 91.8277° |
| revolutions per day: | 15.33555663 |
| mean anomaly at epoch: | 356.5919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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