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 68920U 26145.39196897 +.00000000 +00000-0 +43619-3 0 00004
2 68920 51.8734 177.7247 0009321 60.2081 299.9829 15.33228809 01
| Epoch (UTC): | 25 May 2026 09:24:26 |
| Eccentricity: | 0.0009321 |
| inclination: | 51.8734° |
| perigee height: | 460 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 177.7247° |
| argument of perigee: | 60.2081° |
| revolutions per day: | 15.33228809 |
| mean anomaly at epoch: | 299.9829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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