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 35635U 26053.67633453 +.00000000 +00000-0 +43693-4 0 00007
2 35635 82.9554 114.1192 0018260 223.3414 256.6240 13.89939330 05
| Epoch (UTC): | 22 February 2026 16:13:55 |
| Eccentricity: | 0.0018260 |
| inclination: | 82.9554° |
| perigee height: | 916 km |
| apogee height: | 942 km |
| right ascension of ascending node: | 114.1192° |
| argument of perigee: | 223.3414° |
| revolutions per day: | 13.89939330 |
| mean anomaly at epoch: | 256.6240° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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