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 25682U 26070.85197073 +.00000000 +00000-0 +12162-3 0 00006
2 25682 97.8608 78.9465 0001681 81.1925 39.9522 14.63824062 00
| Epoch (UTC): | 11 March 2026 20:26:50 |
| Eccentricity: | 0.0001681 |
| inclination: | 97.8608° |
| perigee height: | 680 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 78.9465° |
| argument of perigee: | 81.1925° |
| revolutions per day: | 14.63824062 |
| mean anomaly at epoch: | 39.9522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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