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 45447U 26145.40856635 +.00000000 +00000-0 +62126-3 0 00002
2 45447 87.8916 25.6013 0002068 82.9639 277.1724 13.11418272 05
| Epoch (UTC): | 25 May 2026 09:48:20 |
| Eccentricity: | 0.0002068 |
| inclination: | 87.8916° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6013° |
| argument of perigee: | 82.9639° |
| revolutions per day: | 13.11418272 |
| mean anomaly at epoch: | 277.1724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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