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 59074U 26145.53326291 +.00000000 +00000-0 +21617-4 0 00008
2 59074 42.9997 236.7413 0001466 275.1944 84.8741 15.27579468 08
| Epoch (UTC): | 25 May 2026 12:47:53 |
| Eccentricity: | 0.0001466 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.7413° |
| argument of perigee: | 275.1944° |
| revolutions per day: | 15.27579468 |
| mean anomaly at epoch: | 84.8741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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