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 59106U 26145.37011877 +.00000000 +00000-0 +19031-3 0 00003
2 59106 97.8409 277.9512 0010247 94.2145 266.0249 14.99788991 06
| Epoch (UTC): | 25 May 2026 08:52:58 |
| Eccentricity: | 0.0010247 |
| inclination: | 97.8409° |
| perigee height: | 560 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 277.9512° |
| argument of perigee: | 94.2145° |
| revolutions per day: | 14.99788991 |
| mean anomaly at epoch: | 266.0249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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