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 26535U 26020.01928242 +.00000000 +00000-0 +64818-2 0 00001
2 26535 19.7649 302.5813 5873784 209.2436 98.6241 4.14593032 00
| Epoch (UTC): | 20 January 2026 00:27:46 |
| Eccentricity: | 0.5873784 |
| inclination: | 19.7649° |
| perigee height: | 376 km |
| apogee height: | 19604 km |
| right ascension of ascending node: | 302.5813° |
| argument of perigee: | 209.2436° |
| revolutions per day: | 4.14593032 |
| mean anomaly at epoch: | 98.6241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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