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 26715U 26140.35602919 +.00000000 +00000-0 +00000-0 0 00002
2 26715 11.5136 19.9409 0038254 179.3057 16.8904 1.00275316 09
| Epoch (UTC): | 20 May 2026 08:32:40 |
| Eccentricity: | 0.0038254 |
| inclination: | 11.5136° |
| perigee height: | 35624 km |
| apogee height: | 35947 km |
| right ascension of ascending node: | 19.9409° |
| argument of perigee: | 179.3057° |
| revolutions per day: | 1.00275316 |
| mean anomaly at epoch: | 16.8904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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