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 44772U 26145.51643939 +.00000000 +00000-0 +43114-3 0 00001
2 44772 53.0423 160.6925 0002442 65.2966 294.8306 15.73148638 06
| Epoch (UTC): | 25 May 2026 12:23:40 |
| Eccentricity: | 0.0002442 |
| inclination: | 53.0423° |
| perigee height: | 348 km |
| apogee height: | 352 km |
| right ascension of ascending node: | 160.6925° |
| argument of perigee: | 65.2966° |
| revolutions per day: | 15.73148638 |
| mean anomaly at epoch: | 294.8306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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