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 69044U 26145.58335647 +.00000000 +00000-0 -26046-1 0 00005
2 69044 97.2847 0.3496 0001738 95.7509 189.7382 15.60023919 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001738 |
| inclination: | 97.2847° |
| perigee height: | 386 km |
| apogee height: | 389 km |
| right ascension of ascending node: | 0.3496° |
| argument of perigee: | 95.7509° |
| revolutions per day: | 15.60023919 |
| mean anomaly at epoch: | 189.7382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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