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 63173U 26145.57767293 +.00000000 +00000-0 +11376-3 0 00008
2 63173 88.9689 302.9075 0011960 23.6638 336.5061 13.51013824 03
| Epoch (UTC): | 25 May 2026 13:51:50 |
| Eccentricity: | 0.0011960 |
| inclination: | 88.9689° |
| perigee height: | 1060 km |
| apogee height: | 1077 km |
| right ascension of ascending node: | 302.9075° |
| argument of perigee: | 23.6638° |
| revolutions per day: | 13.51013824 |
| mean anomaly at epoch: | 336.5061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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