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 40021U 26145.41174326 +.00000000 +00000-0 +10765-2 0 00007
2 40021 98.0493 201.4574 0006086 156.7264 203.4268 15.59914468 03
| Epoch (UTC): | 25 May 2026 09:52:54 |
| Eccentricity: | 0.0006086 |
| inclination: | 98.0493° |
| perigee height: | 384 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 201.4574° |
| argument of perigee: | 156.7264° |
| revolutions per day: | 15.59914468 |
| mean anomaly at epoch: | 203.4268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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