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 63170U 26145.60340891 +.00000000 +00000-0 +19611-3 0 00000
2 63170 88.9691 303.0631 0016051 18.9521 341.2224 13.51030760 09
| Epoch (UTC): | 25 May 2026 14:28:54 |
| Eccentricity: | 0.0016051 |
| inclination: | 88.9691° |
| perigee height: | 1057 km |
| apogee height: | 1080 km |
| right ascension of ascending node: | 303.0631° |
| argument of perigee: | 18.9521° |
| revolutions per day: | 13.51030760 |
| mean anomaly at epoch: | 341.2224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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