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 59506U 26145.58443454 +.00000000 +00000-0 +68212-4 0 00006
2 59506 43.0014 258.5439 0001339 269.9093 90.1605 15.27584106 09
| Epoch (UTC): | 25 May 2026 14:01:35 |
| Eccentricity: | 0.0001339 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 258.5439° |
| argument of perigee: | 269.9093° |
| revolutions per day: | 15.27584106 |
| mean anomaly at epoch: | 90.1605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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