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 65606U 26145.62885274 +.00000000 +00000-0 +21863-3 0 00009
2 65606 97.4462 214.2058 0002153 129.8819 230.2598 15.05655545 08
| Epoch (UTC): | 25 May 2026 15:05:32 |
| Eccentricity: | 0.0002153 |
| inclination: | 97.4462° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 214.2058° |
| argument of perigee: | 129.8819° |
| revolutions per day: | 15.05655545 |
| mean anomaly at epoch: | 230.2598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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