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 63205U 26145.59128337 +.00000000 +00000-0 +31736-3 0 00008
2 63205 42.0186 227.0792 0004115 345.8215 14.2495 15.02904672 08
| Epoch (UTC): | 25 May 2026 14:11:26 |
| Eccentricity: | 0.0004115 |
| inclination: | 42.0186° |
| perigee height: | 555 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 227.0792° |
| argument of perigee: | 345.8215° |
| revolutions per day: | 15.02904672 |
| mean anomaly at epoch: | 14.2495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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