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 44941U 26145.60999878 +.00000000 +00000-0 +10191-2 0 00003
2 44941 53.1543 317.1097 0002851 280.8362 79.2327 15.52375919 05
| Epoch (UTC): | 25 May 2026 14:38:23 |
| Eccentricity: | 0.0002851 |
| inclination: | 53.1543° |
| perigee height: | 408 km |
| apogee height: | 412 km |
| right ascension of ascending node: | 317.1097° |
| argument of perigee: | 280.8362° |
| revolutions per day: | 15.52375919 |
| mean anomaly at epoch: | 79.2327° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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