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 65600U 26145.42115738 +.00000000 +00000-0 +18658-3 0 00000
2 65600 97.4466 213.8672 0001514 162.8016 197.3263 15.05655931 00
| Epoch (UTC): | 25 May 2026 10:06:27 |
| Eccentricity: | 0.0001514 |
| inclination: | 97.4466° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 213.8672° |
| argument of perigee: | 162.8016° |
| revolutions per day: | 15.05655931 |
| mean anomaly at epoch: | 197.3263° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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