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 26088.19336836 +.00000000 +00000-0 +15141-3 0 00008
2 40715 97.6587 316.4561 0004779 332.8229 27.2736 14.85644771 07
| Epoch (UTC): | 29 March 2026 04:38:27 |
| Eccentricity: | 0.0004779 |
| inclination: | 97.6587° |
| perigee height: | 608 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 316.4561° |
| argument of perigee: | 332.8229° |
| revolutions per day: | 14.85644771 |
| mean anomaly at epoch: | 27.2736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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