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 45131U 26145.47599882 +.00000000 +00000-0 -22704-2 0 00005
2 45131 87.8534 57.4051 0002848 73.4147 286.7292 13.09455461 05
| Epoch (UTC): | 25 May 2026 11:25:26 |
| Eccentricity: | 0.0002848 |
| inclination: | 87.8534° |
| perigee height: | 1223 km |
| apogee height: | 1227 km |
| right ascension of ascending node: | 57.4051° |
| argument of perigee: | 73.4147° |
| revolutions per day: | 13.09455461 |
| mean anomaly at epoch: | 286.7292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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