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 66414U 26145.37594992 +.00000000 +00000-0 +92369-4 0 00003
2 66414 50.0067 17.6775 0001156 57.4155 302.6829 13.29319582 07
| Epoch (UTC): | 25 May 2026 09:01:22 |
| Eccentricity: | 0.0001156 |
| inclination: | 50.0067° |
| perigee height: | 1148 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 17.6775° |
| argument of perigee: | 57.4155° |
| revolutions per day: | 13.29319582 |
| mean anomaly at epoch: | 302.6829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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