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 63172U 26145.60656037 +.00000000 +00000-0 +34453-4 0 00006
2 63172 88.9693 302.7990 0011594 28.4135 331.7646 13.51012463 03
| Epoch (UTC): | 25 May 2026 14:33:26 |
| Eccentricity: | 0.0011594 |
| inclination: | 88.9693° |
| perigee height: | 1060 km |
| apogee height: | 1077 km |
| right ascension of ascending node: | 302.7990° |
| argument of perigee: | 28.4135° |
| revolutions per day: | 13.51012463 |
| mean anomaly at epoch: | 331.7646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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