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 40701U 26145.62112097 +.00000000 +00000-0 +43850-3 0 00004
2 40701 97.6920 337.6524 0007563 275.1794 84.8591 15.45034445 03
| Epoch (UTC): | 25 May 2026 14:54:24 |
| Eccentricity: | 0.0007563 |
| inclination: | 97.6920° |
| perigee height: | 426 km |
| apogee height: | 436 km |
| right ascension of ascending node: | 337.6524° |
| argument of perigee: | 275.1794° |
| revolutions per day: | 15.45034445 |
| mean anomaly at epoch: | 84.8591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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