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 36590U 26145.38561060 +.00000000 +00000-0 +00000-0 0 00003
2 36590 4.4644 61.6175 0008424 344.3015 55.4846 1.00273576 04
| Epoch (UTC): | 25 May 2026 09:15:16 |
| Eccentricity: | 0.0008424 |
| inclination: | 4.4644° |
| perigee height: | 35751 km |
| apogee height: | 35822 km |
| right ascension of ascending node: | 61.6175° |
| argument of perigee: | 344.3015° |
| revolutions per day: | 1.00273576 |
| mean anomaly at epoch: | 55.4846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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