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 56148U 26145.39786582 +.00000000 +00000-0 +83209-5 0 00000
2 56148 43.0018 37.0840 0000812 251.6541 108.4222 15.27576418 04
| Epoch (UTC): | 25 May 2026 09:32:55 |
| Eccentricity: | 0.0000812 |
| inclination: | 43.0018° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 37.0840° |
| argument of perigee: | 251.6541° |
| revolutions per day: | 15.27576418 |
| mean anomaly at epoch: | 108.4222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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