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 40715U 26145.57620130 +.00000000 +00000-0 +51650-4 0 00003
2 40715 97.6492 11.6344 0006730 119.1303 241.0587 14.85706902 08
| Epoch (UTC): | 25 May 2026 13:49:43 |
| Eccentricity: | 0.0006730 |
| inclination: | 97.6492° |
| perigee height: | 607 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 11.6344° |
| argument of perigee: | 119.1303° |
| revolutions per day: | 14.85706902 |
| mean anomaly at epoch: | 241.0587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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