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 63171U 26145.59819113 +.00000000 +00000-0 +53339-4 0 00003
2 63171 88.9690 302.9340 0013598 22.6953 337.4797 13.51014796 01
| Epoch (UTC): | 25 May 2026 14:21:23 |
| Eccentricity: | 0.0013598 |
| inclination: | 88.9690° |
| perigee height: | 1058 km |
| apogee height: | 1079 km |
| right ascension of ascending node: | 302.9340° |
| argument of perigee: | 22.6953° |
| revolutions per day: | 13.51014796 |
| mean anomaly at epoch: | 337.4797° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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