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 66259U 26145.41042294 +.00000000 +00000-0 +66881-3 0 00007
2 66259 53.1588 287.4682 0001075 90.5367 269.5757 15.30212983 05
| Epoch (UTC): | 25 May 2026 09:51:00 |
| Eccentricity: | 0.0001075 |
| inclination: | 53.1588° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 287.4682° |
| argument of perigee: | 90.5367° |
| revolutions per day: | 15.30212983 |
| mean anomaly at epoch: | 269.5757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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