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 59622U 26145.53442244 +.00000000 +00000-0 -36069-5 0 00003
2 59622 43.0033 320.5925 0000993 275.9306 84.1433 15.27572695 00
| Epoch (UTC): | 25 May 2026 12:49:34 |
| Eccentricity: | 0.0000993 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.5925° |
| argument of perigee: | 275.9306° |
| revolutions per day: | 15.27572695 |
| mean anomaly at epoch: | 84.1433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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