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 26156.87777985 +.00000000 +00000-0 +12436-3 0 00006
2 36089 98.4559 134.5519 0079121 76.1045 284.8935 14.52397630 08
| Epoch (UTC): | 05 June 2026 21:04:00 |
| Eccentricity: | 0.0079121 |
| inclination: | 98.4559° |
| perigee height: | 662 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 134.5519° |
| argument of perigee: | 76.1045° |
| revolutions per day: | 14.52397630 |
| mean anomaly at epoch: | 284.8935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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