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 26150.71796639 +.00000000 +00000-0 +36542-3 0 00009
2 36796 98.0969 56.8311 0013049 91.0557 269.2163 15.04754072 06
| Epoch (UTC): | 30 May 2026 17:13:52 |
| Eccentricity: | 0.0013049 |
| inclination: | 98.0969° |
| perigee height: | 543 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 56.8311° |
| argument of perigee: | 91.0557° |
| revolutions per day: | 15.04754072 |
| mean anomaly at epoch: | 269.2163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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