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 62185U 26145.64921544 +.00000000 +00000-0 +43271-4 0 00009
2 62185 50.0060 349.8039 0056565 79.2675 281.4573 13.60152314 00
| Epoch (UTC): | 25 May 2026 15:34:52 |
| Eccentricity: | 0.0056565 |
| inclination: | 50.0060° |
| perigee height: | 993 km |
| apogee height: | 1077 km |
| right ascension of ascending node: | 349.8039° |
| argument of perigee: | 79.2675° |
| revolutions per day: | 13.60152314 |
| mean anomaly at epoch: | 281.4573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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