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 36796U 26044.68996855 +.00000000 +00000-0 +29495-3 0 00008
2 36796 98.1045 305.7722 0012902 86.0254 274.2445 15.03759125 01
| Epoch (UTC): | 13 February 2026 16:33:33 |
| Eccentricity: | 0.0012902 |
| inclination: | 98.1045° |
| perigee height: | 546 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 305.7722° |
| argument of perigee: | 86.0254° |
| revolutions per day: | 15.03759125 |
| mean anomaly at epoch: | 274.2445° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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