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 25338U 26040.58386439 +.00000000 +00000-0 +89109-4 0 00003
2 25338 98.5187 64.5971 0010294 8.1670 351.9676 14.27100828 01
| Epoch (UTC): | 09 February 2026 14:00:45 |
| Eccentricity: | 0.0010294 |
| inclination: | 98.5187° |
| perigee height: | 794 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 64.5971° |
| argument of perigee: | 8.1670° |
| revolutions per day: | 14.27100828 |
| mean anomaly at epoch: | 351.9676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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