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 26074.94228529 +.00000000 +00000-0 +80944-4 0 00002
2 25940 98.8519 81.8647 0003834 274.3160 85.7588 14.36964231 07
| Epoch (UTC): | 15 March 2026 22:36:53 |
| Eccentricity: | 0.0003834 |
| inclination: | 98.8519° |
| perigee height: | 766 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 81.8647° |
| argument of perigee: | 274.3160° |
| revolutions per day: | 14.36964231 |
| mean anomaly at epoch: | 85.7588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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