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 69074U 26145.70109889 +.00000000 +00000-0 +64104-4 0 00008
2 69074 88.9868 344.1934 0003328 159.0140 201.1186 14.18043389 09
| Epoch (UTC): | 25 May 2026 16:49:34 |
| Eccentricity: | 0.0003328 |
| inclination: | 88.9868° |
| perigee height: | 830 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 344.1934° |
| argument of perigee: | 159.0140° |
| revolutions per day: | 14.18043389 |
| mean anomaly at epoch: | 201.1186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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