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 59266U 26145.33110748 +.00000000 +00000-0 +67494-4 0 00000
2 59266 53.1601 184.9381 0000599 80.9011 279.2058 15.30195194 03
| Epoch (UTC): | 25 May 2026 07:56:47 |
| Eccentricity: | 0.0000599 |
| inclination: | 53.1601° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.9381° |
| argument of perigee: | 80.9011° |
| revolutions per day: | 15.30195194 |
| mean anomaly at epoch: | 279.2058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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