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 63897U 26145.25265308 +.00000000 +00000-0 +65595-3 0 00008
2 63897 43.0012 104.1344 0000701 227.7828 132.2964 15.27593786 06
| Epoch (UTC): | 25 May 2026 06:03:49 |
| Eccentricity: | 0.0000701 |
| inclination: | 43.0012° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 104.1344° |
| argument of perigee: | 227.7828° |
| revolutions per day: | 15.27593786 |
| mean anomaly at epoch: | 132.2964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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