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 45272U 26088.20685968 +.00000000 +00000-0 +35289-2 0 00000
2 45272 82.6434 78.0415 0177816 112.0758 249.9389 13.79229982 04
| Epoch (UTC): | 29 March 2026 04:57:52 |
| Eccentricity: | 0.0177816 |
| inclination: | 82.6434° |
| perigee height: | 836 km |
| apogee height: | 1097 km |
| right ascension of ascending node: | 78.0415° |
| argument of perigee: | 112.0758° |
| revolutions per day: | 13.79229982 |
| mean anomaly at epoch: | 249.9389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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