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 26095.90717113 +.00000000 +00000-0 +13148-3 0 00000
2 36089 98.4519 73.1310 0076688 262.3400 96.9081 14.52360244 05
| Epoch (UTC): | 05 April 2026 21:46:19 |
| Eccentricity: | 0.0076688 |
| inclination: | 98.4519° |
| perigee height: | 664 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 73.1310° |
| argument of perigee: | 262.3400° |
| revolutions per day: | 14.52360244 |
| mean anomaly at epoch: | 96.9081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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