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 68930U 26145.46220759 +.00000000 +00000-0 +38716-3 0 00000
2 68930 51.8768 177.4522 0011081 56.9779 303.2269 15.33122047 08
| Epoch (UTC): | 25 May 2026 11:05:34 |
| Eccentricity: | 0.0011081 |
| inclination: | 51.8768° |
| perigee height: | 459 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 177.4522° |
| argument of perigee: | 56.9779° |
| revolutions per day: | 15.33122047 |
| mean anomaly at epoch: | 303.2269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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