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 00045U 26022.30851038 +.00000000 +00000-0 +23997-3 0 00005
2 00045 66.6936 26.0426 0256356 265.8146 91.3623 14.35838639 00
| Epoch (UTC): | 22 January 2026 07:24:15 |
| Eccentricity: | 0.0256356 |
| inclination: | 66.6936° |
| perigee height: | 589 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 26.0426° |
| argument of perigee: | 265.8146° |
| revolutions per day: | 14.35838639 |
| mean anomaly at epoch: | 91.3623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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