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 65662U 26145.12444525 +.00000000 +00000-0 +23067-3 0 00004
2 65662 97.4471 189.0509 0002195 140.8501 219.2885 15.05654816 03
| Epoch (UTC): | 25 May 2026 02:59:12 |
| Eccentricity: | 0.0002195 |
| inclination: | 97.4471° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 189.0509° |
| argument of perigee: | 140.8501° |
| revolutions per day: | 15.05654816 |
| mean anomaly at epoch: | 219.2885° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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