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 66715U 26145.48462912 +.00000000 +00000-0 +29205-3 0 00003
2 66715 97.4193 219.5325 0003359 69.2799 290.8796 15.20169689 07
| Epoch (UTC): | 25 May 2026 11:37:51 |
| Eccentricity: | 0.0003359 |
| inclination: | 97.4193° |
| perigee height: | 503 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 219.5325° |
| argument of perigee: | 69.2799° |
| revolutions per day: | 15.20169689 |
| mean anomaly at epoch: | 290.8796° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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