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 68722U 26145.58335647 +.00000000 +00000-0 -41670-1 0 00007
2 68722 53.1603 36.7831 0001058 86.0043 51.6499 15.40742011 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001058 |
| inclination: | 53.1603° |
| perigee height: | 443 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 36.7831° |
| argument of perigee: | 86.0043° |
| revolutions per day: | 15.40742011 |
| mean anomaly at epoch: | 51.6499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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