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 59853U 26145.51475625 +.00000000 +00000-0 +47290-5 0 00003
2 59853 43.0002 200.7109 0001337 287.7063 72.3642 15.27576324 03
| Epoch (UTC): | 25 May 2026 12:21:14 |
| Eccentricity: | 0.0001337 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.7109° |
| argument of perigee: | 287.7063° |
| revolutions per day: | 15.27576324 |
| mean anomaly at epoch: | 72.3642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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