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 45764U 26145.58335647 +.00000000 +00000-0 +14260-2 0 00003
2 45764 53.0454 195.2432 0007141 325.0931 71.5807 15.59236395 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0007141 |
| inclination: | 53.0454° |
| perigee height: | 385 km |
| apogee height: | 395 km |
| right ascension of ascending node: | 195.2432° |
| argument of perigee: | 325.0931° |
| revolutions per day: | 15.59236395 |
| mean anomaly at epoch: | 71.5807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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