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 59078U 26145.60378984 +.00000000 +00000-0 +53052-3 0 00003
2 59078 42.9986 236.4075 0001386 278.5822 81.4873 15.27581643 01
| Epoch (UTC): | 25 May 2026 14:29:27 |
| Eccentricity: | 0.0001386 |
| inclination: | 42.9986° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.4075° |
| argument of perigee: | 278.5822° |
| revolutions per day: | 15.27581643 |
| mean anomaly at epoch: | 81.4873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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