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 26066.58657196 +.00000000 +00000-0 +12145-3 0 00006
2 25940 98.8520 73.2722 0004015 305.5390 54.5421 14.36959450 09
| Epoch (UTC): | 07 March 2026 14:04:39 |
| Eccentricity: | 0.0004015 |
| inclination: | 98.8520° |
| perigee height: | 766 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 73.2722° |
| argument of perigee: | 305.5390° |
| revolutions per day: | 14.36959450 |
| mean anomaly at epoch: | 54.5421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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