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 36799U 26150.40915481 +.00000000 +00000-0 +85772-3 0 00005
2 36799 98.0704 95.3919 0001177 24.7260 335.4035 15.30958871 07
| Epoch (UTC): | 30 May 2026 09:49:10 |
| Eccentricity: | 0.0001177 |
| inclination: | 98.0704° |
| perigee height: | 472 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 95.3919° |
| argument of perigee: | 24.7260° |
| revolutions per day: | 15.30958871 |
| mean anomaly at epoch: | 335.4035° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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