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 44768U 26145.60691669 +.00000000 +00000-0 +86903-3 0 00002
2 44768 53.1564 217.6182 0001554 22.4853 337.6223 15.47065265 08
| Epoch (UTC): | 25 May 2026 14:33:57 |
| Eccentricity: | 0.0001554 |
| inclination: | 53.1564° |
| perigee height: | 424 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 217.6182° |
| argument of perigee: | 22.4853° |
| revolutions per day: | 15.47065265 |
| mean anomaly at epoch: | 337.6223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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