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 40959U 26145.60467152 +.00000000 +00000-0 +74406-4 0 00004
2 40959 97.6622 141.5225 0016552 348.4730 11.6100 14.77354663 04
| Epoch (UTC): | 25 May 2026 14:30:43 |
| Eccentricity: | 0.0016552 |
| inclination: | 97.6622° |
| perigee height: | 626 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 141.5225° |
| argument of perigee: | 348.4730° |
| revolutions per day: | 14.77354663 |
| mean anomaly at epoch: | 11.6100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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