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 26150.57749507 +.00000000 +00000-0 +37398-3 0 00002
2 40022 98.1229 154.3665 0004587 279.4772 80.5938 15.10636578 08
| Epoch (UTC): | 30 May 2026 13:51:35 |
| Eccentricity: | 0.0004587 |
| inclination: | 98.1229° |
| perigee height: | 531 km |
| apogee height: | 537 km |
| right ascension of ascending node: | 154.3665° |
| argument of perigee: | 279.4772° |
| revolutions per day: | 15.10636578 |
| mean anomaly at epoch: | 80.5938° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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