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 44233U 26145.41043654 +.00000000 +00000-0 +17449-3 0 00002
2 44233 36.9956 129.1725 0005746 222.7233 137.3063 15.01525160 05
| Epoch (UTC): | 25 May 2026 09:51:01 |
| Eccentricity: | 0.0005746 |
| inclination: | 36.9956° |
| perigee height: | 558 km |
| apogee height: | 566 km |
| right ascension of ascending node: | 129.1725° |
| argument of perigee: | 222.7233° |
| revolutions per day: | 15.01525160 |
| mean anomaly at epoch: | 137.3063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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