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 68793U 26145.36842153 +.00000000 +00000-0 +28267-3 0 00004
2 68793 97.5033 295.2186 0015820 176.7164 183.4170 15.06858332 08
| Epoch (UTC): | 25 May 2026 08:50:31 |
| Eccentricity: | 0.0015820 |
| inclination: | 97.5033° |
| perigee height: | 535 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 295.2186° |
| argument of perigee: | 176.7164° |
| revolutions per day: | 15.06858332 |
| mean anomaly at epoch: | 183.4170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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