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 26145.56335578 +.00000000 +00000-0 +00000-0 0 00005
2 25258 11.1053 22.9055 0004505 273.7003 302.7322 1.00273678 07
| Epoch (UTC): | 25 May 2026 13:31:13 |
| Eccentricity: | 0.0004505 |
| inclination: | 11.1053° |
| perigee height: | 35767 km |
| apogee height: | 35805 km |
| right ascension of ascending node: | 22.9055° |
| argument of perigee: | 273.7003° |
| revolutions per day: | 1.00273678 |
| mean anomaly at epoch: | 302.7322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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