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 68938U 26145.44754968 +.00000000 +00000-0 +55923-3 0 00009
2 68938 51.8722 177.3454 0007880 55.2283 304.9443 15.34576912 00
| Epoch (UTC): | 25 May 2026 10:44:28 |
| Eccentricity: | 0.0007880 |
| inclination: | 51.8722° |
| perigee height: | 457 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 177.3454° |
| argument of perigee: | 55.2283° |
| revolutions per day: | 15.34576912 |
| mean anomaly at epoch: | 304.9443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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