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 69046U 26145.57680160 +.00000000 +00000-0 +63293-3 0 00005
2 69046 97.2847 0.3871 0001341 75.0737 285.0677 15.75214339 06
| Epoch (UTC): | 25 May 2026 13:50:35 |
| Eccentricity: | 0.0001341 |
| inclination: | 97.2847° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 0.3871° |
| argument of perigee: | 75.0737° |
| revolutions per day: | 15.75214339 |
| mean anomaly at epoch: | 285.0677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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