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 25986U 26088.23234617 +.00000000 +00000-0 +37332-3 0 00006
2 25986 45.0383 187.0250 0003647 305.4305 54.6203 14.37825140 03
| Epoch (UTC): | 29 March 2026 05:34:34 |
| Eccentricity: | 0.0003647 |
| inclination: | 45.0383° |
| perigee height: | 763 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 187.0250° |
| argument of perigee: | 305.4305° |
| revolutions per day: | 14.37825140 |
| mean anomaly at epoch: | 54.6203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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