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 25985U 26087.70445896 +.00000000 +00000-0 +37647-3 0 00008
2 25985 45.0388 189.0020 0002098 0.5616 359.5235 14.37919473 06
| Epoch (UTC): | 28 March 2026 16:54:25 |
| Eccentricity: | 0.0002098 |
| inclination: | 45.0388° |
| perigee height: | 764 km |
| apogee height: | 767 km |
| right ascension of ascending node: | 189.0020° |
| argument of perigee: | 0.5616° |
| revolutions per day: | 14.37919473 |
| mean anomaly at epoch: | 359.5235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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