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 45920U 26145.60675947 +.00000000 +00000-0 +00000-0 0 00005
2 45920 0.0121 300.5518 0000949 121.2037 156.0647 1.00273984 09
| Epoch (UTC): | 25 May 2026 14:33:44 |
| Eccentricity: | 0.0000949 |
| inclination: | 0.0121° |
| perigee height: | 35782 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 300.5518° |
| argument of perigee: | 121.2037° |
| revolutions per day: | 1.00273984 |
| mean anomaly at epoch: | 156.0647° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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