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 25868U 26109.43859486 +.00000000 +00000-0 +89657-3 0 00005
2 25868 28.4465 136.8722 4345329 92.8297 316.1067 6.85275345 05
| Epoch (UTC): | 19 April 2026 10:31:34 |
| Eccentricity: | 0.4345329 |
| inclination: | 28.4465° |
| perigee height: | 242 km |
| apogee height: | 10418 km |
| right ascension of ascending node: | 136.8722° |
| argument of perigee: | 92.8297° |
| revolutions per day: | 6.85275345 |
| mean anomaly at epoch: | 316.1067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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