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 59364U 26145.44987314 +.00000000 +00000-0 -21113-4 0 00001
2 59364 43.0005 174.9925 0001316 279.3177 80.7526 15.27574460 04
| Epoch (UTC): | 25 May 2026 10:47:49 |
| Eccentricity: | 0.0001316 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 174.9925° |
| argument of perigee: | 279.3177° |
| revolutions per day: | 15.27574460 |
| mean anomaly at epoch: | 80.7526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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