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 59361U 26145.47041073 +.00000000 +00000-0 +11716-4 0 00001
2 59361 42.9997 186.3901 0001474 270.3172 89.7510 15.27582118 02
| Epoch (UTC): | 25 May 2026 11:17:23 |
| Eccentricity: | 0.0001474 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.3901° |
| argument of perigee: | 270.3172° |
| revolutions per day: | 15.27582118 |
| mean anomaly at epoch: | 89.7510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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