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 36089U 26037.96642869 +.00000000 +00000-0 +16982-3 0 00006
2 36089 98.4425 14.8247 0079264 79.8296 281.1828 14.52287586 03
| Epoch (UTC): | 06 February 2026 23:11:39 |
| Eccentricity: | 0.0079264 |
| inclination: | 98.4425° |
| perigee height: | 662 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 14.8247° |
| argument of perigee: | 79.8296° |
| revolutions per day: | 14.52287586 |
| mean anomaly at epoch: | 281.1828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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