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 61614U 26145.58132962 +.00000000 +00000-0 +21989-3 0 00007
2 61614 97.5221 166.5258 0003115 69.9073 290.2486 15.01012769 06
| Epoch (UTC): | 25 May 2026 13:57:06 |
| Eccentricity: | 0.0003115 |
| inclination: | 97.5221° |
| perigee height: | 562 km |
| apogee height: | 566 km |
| right ascension of ascending node: | 166.5258° |
| argument of perigee: | 69.9073° |
| revolutions per day: | 15.01012769 |
| mean anomaly at epoch: | 290.2486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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