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 59848U 26145.49901819 +.00000000 +00000-0 +64893-4 0 00000
2 59848 42.9995 193.6663 0001386 282.7089 77.3608 15.27572349 08
| Epoch (UTC): | 25 May 2026 11:58:35 |
| Eccentricity: | 0.0001386 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.6663° |
| argument of perigee: | 282.7089° |
| revolutions per day: | 15.27572349 |
| mean anomaly at epoch: | 77.3608° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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