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 14452U 26039.58191979 +.00000000 +00000-0 +74885-4 0 00004
2 14452 81.1625 127.0231 0089484 215.5787 143.9408 14.27239643 05
| Epoch (UTC): | 08 February 2026 13:57:57 |
| Eccentricity: | 0.0089484 |
| inclination: | 81.1625° |
| perigee height: | 737 km |
| apogee height: | 865 km |
| right ascension of ascending node: | 127.0231° |
| argument of perigee: | 215.5787° |
| revolutions per day: | 14.27239643 |
| mean anomaly at epoch: | 143.9408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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