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 69078U 26145.62884617 +.00000000 +00000-0 +32742-4 0 00005
2 69078 88.9868 344.2011 0003744 158.9128 201.2217 14.18144338 08
| Epoch (UTC): | 25 May 2026 15:05:32 |
| Eccentricity: | 0.0003744 |
| inclination: | 88.9868° |
| perigee height: | 829 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 344.2011° |
| argument of perigee: | 158.9128° |
| revolutions per day: | 14.18144338 |
| mean anomaly at epoch: | 201.2217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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