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 63188U 26145.58380095 +.00000000 +00000-0 +11997-2 0 00004
2 63188 42.9981 216.4924 0001349 40.9523 319.1446 15.70822332 00
| Epoch (UTC): | 25 May 2026 14:00:40 |
| Eccentricity: | 0.0001349 |
| inclination: | 42.9981° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 216.4924° |
| argument of perigee: | 40.9523° |
| revolutions per day: | 15.70822332 |
| mean anomaly at epoch: | 319.1446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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