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 25258U 26140.46364006 +.00000000 +00000-0 +00000-0 0 00007
2 25258 11.0993 22.9345 0004899 271.8812 263.5732 1.00273712 02
| Epoch (UTC): | 20 May 2026 11:07:38 |
| Eccentricity: | 0.0004899 |
| inclination: | 11.0993° |
| perigee height: | 35765 km |
| apogee height: | 35807 km |
| right ascension of ascending node: | 22.9345° |
| argument of perigee: | 271.8812° |
| revolutions per day: | 1.00273712 |
| mean anomaly at epoch: | 263.5732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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