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 25940U 26073.61929904 +.00000000 +00000-0 +10336-3 0 00007
2 25940 98.8518 80.5043 0003852 279.5123 80.5627 14.36963835 04
| Epoch (UTC): | 14 March 2026 14:51:47 |
| Eccentricity: | 0.0003852 |
| inclination: | 98.8518° |
| perigee height: | 766 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 80.5043° |
| argument of perigee: | 279.5123° |
| revolutions per day: | 14.36963835 |
| mean anomaly at epoch: | 80.5627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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