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 68140U 26145.74056242 +.00000000 +00000-0 +17517-3 0 00004
2 68140 34.9925 42.3525 0003029 186.8048 173.2616 14.91722507 07
| Epoch (UTC): | 25 May 2026 17:46:24 |
| Eccentricity: | 0.0003029 |
| inclination: | 34.9925° |
| perigee height: | 590 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 42.3525° |
| argument of perigee: | 186.8048° |
| revolutions per day: | 14.91722507 |
| mean anomaly at epoch: | 173.2616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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