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 25940U 26053.77442051 +.00000000 +00000-0 +83593-4 0 00001
2 25940 98.8516 60.0983 0004602 348.4389 11.6690 14.36951581 02
| Epoch (UTC): | 22 February 2026 18:35:09 |
| Eccentricity: | 0.0004602 |
| inclination: | 98.8516° |
| perigee height: | 765 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 60.0983° |
| argument of perigee: | 348.4389° |
| revolutions per day: | 14.36951581 |
| mean anomaly at epoch: | 11.6690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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