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 45457U 26145.62219122 +.00000000 +00000-0 -13186-2 0 00003
2 45457 87.8927 25.5207 0002166 87.6637 272.4739 13.11417290 04
| Epoch (UTC): | 25 May 2026 14:55:57 |
| Eccentricity: | 0.0002166 |
| inclination: | 87.8927° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5207° |
| argument of perigee: | 87.6637° |
| revolutions per day: | 13.11417290 |
| mean anomaly at epoch: | 272.4739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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