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 68171U 26145.05845044 +.00000000 +00000-0 +92234-3 0 00007
2 68171 53.1589 271.4520 0000954 74.4888 285.6220 15.34399759 04
| Epoch (UTC): | 25 May 2026 01:24:10 |
| Eccentricity: | 0.0000954 |
| inclination: | 53.1589° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 271.4520° |
| argument of perigee: | 74.4888° |
| revolutions per day: | 15.34399759 |
| mean anomaly at epoch: | 285.6220° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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