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 26088.07461447 +.00000000 +00000-0 +91959-3 0 00000
2 36799 98.0655 27.7471 0003635 128.8120 231.3443 15.28514657 00
| Epoch (UTC): | 29 March 2026 01:47:26 |
| Eccentricity: | 0.0003635 |
| inclination: | 98.0655° |
| perigee height: | 478 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 27.7471° |
| argument of perigee: | 128.8120° |
| revolutions per day: | 15.28514657 |
| mean anomaly at epoch: | 231.3443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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