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 25635U 26054.52359332 +.00000000 +00000-0 +12911-3 0 00000
2 25635 96.4800 347.8705 0131834 190.4539 169.3916 14.51660746 00
| Epoch (UTC): | 23 February 2026 12:33:58 |
| Eccentricity: | 0.0131834 |
| inclination: | 96.4800° |
| perigee height: | 627 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 347.8705° |
| argument of perigee: | 190.4539° |
| revolutions per day: | 14.51660746 |
| mean anomaly at epoch: | 169.3916° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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