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 36581U 26145.58840845 +.00000000 +00000-0 +00000-0 0 00006
2 36581 1.4120 83.8093 0004141 344.6504 50.0840 1.00275677 02
| Epoch (UTC): | 25 May 2026 14:07:18 |
| Eccentricity: | 0.0004141 |
| inclination: | 1.4120° |
| perigee height: | 35768 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 83.8093° |
| argument of perigee: | 344.6504° |
| revolutions per day: | 1.00275677 |
| mean anomaly at epoch: | 50.0840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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