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 26071.94815781 +.00000000 +00000-0 +10523-3 0 00006
2 25940 98.8520 78.7857 0003877 285.7485 74.3273 14.36962779 00
| Epoch (UTC): | 12 March 2026 22:45:20 |
| Eccentricity: | 0.0003877 |
| inclination: | 98.8520° |
| perigee height: | 766 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 78.7857° |
| argument of perigee: | 285.7485° |
| revolutions per day: | 14.36962779 |
| mean anomaly at epoch: | 74.3273° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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