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 63896U 26145.35386661 +.00000000 +00000-0 +67514-3 0 00007
2 63896 43.0010 103.1670 0001512 266.5551 93.5128 15.27601554 03
| Epoch (UTC): | 25 May 2026 08:29:34 |
| Eccentricity: | 0.0001512 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.1670° |
| argument of perigee: | 266.5551° |
| revolutions per day: | 15.27601554 |
| mean anomaly at epoch: | 93.5128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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