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 68125U 26145.33521569 +.00000000 +00000-0 +75982-3 0 00001
2 68125 97.2849 106.0295 0000869 103.7411 256.3928 15.33458298 09
| Epoch (UTC): | 25 May 2026 08:02:42 |
| Eccentricity: | 0.0000869 |
| inclination: | 97.2849° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 106.0295° |
| argument of perigee: | 103.7411° |
| revolutions per day: | 15.33458298 |
| mean anomaly at epoch: | 256.3928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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