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 63218U 26145.66159802 +.00000000 +00000-0 +55157-3 0 00004
2 63218 97.3909 41.6356 0002786 157.3029 202.8337 15.33048519 08
| Epoch (UTC): | 25 May 2026 15:52:42 |
| Eccentricity: | 0.0002786 |
| inclination: | 97.3909° |
| perigee height: | 465 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 41.6356° |
| argument of perigee: | 157.3029° |
| revolutions per day: | 15.33048519 |
| mean anomaly at epoch: | 202.8337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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