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 26071.18367105 +.00000000 +00000-0 +13570-3 0 00002
2 25682 97.8608 79.2630 0001677 81.0756 347.0032 14.63824935 02
| Epoch (UTC): | 12 March 2026 04:24:29 |
| Eccentricity: | 0.0001677 |
| inclination: | 97.8608° |
| perigee height: | 680 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 79.2630° |
| argument of perigee: | 81.0756° |
| revolutions per day: | 14.63824935 |
| mean anomaly at epoch: | 347.0032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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