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 25479U 26018.86902137 +.00000000 +00000-0 +31601-3 0 00007
2 25479 45.0084 324.2664 0005305 266.2688 93.7554 14.38731934 04
| Epoch (UTC): | 18 January 2026 20:51:23 |
| Eccentricity: | 0.0005305 |
| inclination: | 45.0084° |
| perigee height: | 759 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 324.2664° |
| argument of perigee: | 266.2688° |
| revolutions per day: | 14.38731934 |
| mean anomaly at epoch: | 93.7554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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