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 26145.31062712 +.00000000 +00000-0 +68657-3 0 00002
2 36799 98.0695 89.8486 0002169 30.8829 329.2537 15.30703160 01
| Epoch (UTC): | 25 May 2026 07:27:18 |
| Eccentricity: | 0.0002169 |
| inclination: | 98.0695° |
| perigee height: | 472 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 89.8486° |
| argument of perigee: | 30.8829° |
| revolutions per day: | 15.30703160 |
| mean anomaly at epoch: | 329.2537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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