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 59858U 26145.59463101 +.00000000 +00000-0 -49298-4 0 00002
2 59858 43.0065 196.2550 0001931 282.2090 77.8545 15.27583966 08
| Epoch (UTC): | 25 May 2026 14:16:16 |
| Eccentricity: | 0.0001931 |
| inclination: | 43.0065° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 196.2550° |
| argument of perigee: | 282.2090° |
| revolutions per day: | 15.27583966 |
| mean anomaly at epoch: | 77.8545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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