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 36089U 26105.82788060 +.00000000 +00000-0 +31569-4 0 00000
2 36089 98.4529 83.1223 0076870 231.5026 127.9258 14.52365665 08
| Epoch (UTC): | 15 April 2026 19:52:08 |
| Eccentricity: | 0.0076870 |
| inclination: | 98.4529° |
| perigee height: | 663 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 83.1223° |
| argument of perigee: | 231.5026° |
| revolutions per day: | 14.52365665 |
| mean anomaly at epoch: | 127.9258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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