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 59897U 26145.12695108 +.00000000 +00000-0 +37730-4 0 00005
2 59897 43.0042 54.0082 0001065 276.6729 83.4001 15.27584124 08
| Epoch (UTC): | 25 May 2026 03:02:48 |
| Eccentricity: | 0.0001065 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 54.0082° |
| argument of perigee: | 276.6729° |
| revolutions per day: | 15.27584124 |
| mean anomaly at epoch: | 83.4001° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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