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 40022U 26103.87263028 +.00000000 +00000-0 +21516-3 0 00007
2 40022 98.1253 104.8179 0007955 79.9164 280.2961 15.10208359 02
| Epoch (UTC): | 13 April 2026 20:56:35 |
| Eccentricity: | 0.0007955 |
| inclination: | 98.1253° |
| perigee height: | 530 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 104.8179° |
| argument of perigee: | 79.9164° |
| revolutions per day: | 15.10208359 |
| mean anomaly at epoch: | 280.2961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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