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 65610U 26145.47100313 +.00000000 +00000-0 +37932-3 0 00005
2 65610 97.4486 213.9549 0001727 175.1821 184.9423 15.05660305 05
| Epoch (UTC): | 25 May 2026 11:18:14 |
| Eccentricity: | 0.0001727 |
| inclination: | 97.4486° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 213.9549° |
| argument of perigee: | 175.1821° |
| revolutions per day: | 15.05660305 |
| mean anomaly at epoch: | 184.9423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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