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 59851U 26145.49677007 +.00000000 +00000-0 +98463-4 0 00003
2 59851 42.9995 200.5775 0001752 282.3633 77.7022 15.27575355 06
| Epoch (UTC): | 25 May 2026 11:55:20 |
| Eccentricity: | 0.0001752 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.5775° |
| argument of perigee: | 282.3633° |
| revolutions per day: | 15.27575355 |
| mean anomaly at epoch: | 77.7022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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