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 26145.18120227 +.00000000 +00000-0 +56181-3 0 00006
2 25669 28.9156 73.1353 7099747 130.2560 317.2064 2.33043330 07
| Epoch (UTC): | 25 May 2026 04:20:55 |
| Eccentricity: | 0.7099747 |
| inclination: | 28.9156° |
| perigee height: | 592 km |
| apogee height: | 34715 km |
| right ascension of ascending node: | 73.1353° |
| argument of perigee: | 130.2560° |
| revolutions per day: | 2.33043330 |
| mean anomaly at epoch: | 317.2064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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