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 36088U 26150.50413316 +.00000000 +00000-0 +18070-3 0 00004
2 36088 98.0037 131.9928 0012359 79.1613 73.1909 14.63673657 01
| Epoch (UTC): | 30 May 2026 12:05:57 |
| Eccentricity: | 0.0012359 |
| inclination: | 98.0037° |
| perigee height: | 673 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 131.9928° |
| argument of perigee: | 79.1613° |
| revolutions per day: | 14.63673657 |
| mean anomaly at epoch: | 73.1909° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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