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 63653U 26145.38290821 +.00000000 +00000-0 +10235-2 0 00000
2 63653 43.0016 292.2952 0001542 280.8284 79.2394 15.27598979 00
| Epoch (UTC): | 25 May 2026 09:11:23 |
| Eccentricity: | 0.0001542 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 292.2952° |
| argument of perigee: | 280.8284° |
| revolutions per day: | 15.27598979 |
| mean anomaly at epoch: | 79.2394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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