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 65114U 26145.61588324 +.00000000 +00000-0 +10822-3 0 00001
2 65114 50.0027 46.2958 0009830 36.9077 323.2470 13.29321787 03
| Epoch (UTC): | 25 May 2026 14:46:52 |
| Eccentricity: | 0.0009830 |
| inclination: | 50.0027° |
| perigee height: | 1142 km |
| apogee height: | 1157 km |
| right ascension of ascending node: | 46.2958° |
| argument of perigee: | 36.9077° |
| revolutions per day: | 13.29321787 |
| mean anomaly at epoch: | 323.2470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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