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 45695U 26144.80251082 +.00000000 +00000-0 +43706-3 0 00008
2 45695 53.0470 11.0978 0006009 92.5788 267.5915 15.66424998 09
| Epoch (UTC): | 24 May 2026 19:15:36 |
| Eccentricity: | 0.0006009 |
| inclination: | 53.0470° |
| perigee height: | 365 km |
| apogee height: | 373 km |
| right ascension of ascending node: | 11.0978° |
| argument of perigee: | 92.5788° |
| revolutions per day: | 15.66424998 |
| mean anomaly at epoch: | 267.5915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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