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 59040U 26144.88184411 +.00000000 +00000-0 +54269-4 0 00003
2 59040 43.0015 312.9935 0001273 274.9326 85.1381 15.27584841 02
| Epoch (UTC): | 24 May 2026 21:09:51 |
| Eccentricity: | 0.0001273 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 312.9935° |
| argument of perigee: | 274.9326° |
| revolutions per day: | 15.27584841 |
| mean anomaly at epoch: | 85.1381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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