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 45338U 26087.46209041 +.00000000 +00000-0 +82305-2 0 00005
2 45338 82.5697 87.8117 0118447 249.6302 109.2100 13.80475043 03
| Epoch (UTC): | 28 March 2026 11:05:24 |
| Eccentricity: | 0.0118447 |
| inclination: | 82.5697° |
| perigee height: | 875 km |
| apogee height: | 1049 km |
| right ascension of ascending node: | 87.8117° |
| argument of perigee: | 249.6302° |
| revolutions per day: | 13.80475043 |
| mean anomaly at epoch: | 109.2100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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