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 25501U 26146.10023388 +.00000000 +00000-0 +00000-0 0 00000
2 25501 11.2807 21.4172 0012509 353.4317 353.0626 0.98175400 03
| Epoch (UTC): | 26 May 2026 02:24:20 |
| Eccentricity: | 0.0012509 |
| inclination: | 11.2807° |
| perigee height: | 36331 km |
| apogee height: | 36438 km |
| right ascension of ascending node: | 21.4172° |
| argument of perigee: | 353.4317° |
| revolutions per day: | 0.98175400 |
| mean anomaly at epoch: | 353.0626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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