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 25669U 26140.46459677 +.00000000 +00000-0 +97322-5 0 00000
2 25669 28.9016 74.7889 7099611 127.6176 320.1899 2.33043083 00
| Epoch (UTC): | 20 May 2026 11:09:01 |
| Eccentricity: | 0.7099611 |
| inclination: | 28.9016° |
| perigee height: | 592 km |
| apogee height: | 34714 km |
| right ascension of ascending node: | 74.7889° |
| argument of perigee: | 127.6176° |
| revolutions per day: | 2.33043083 |
| mean anomaly at epoch: | 320.1899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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