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 56147U 26145.66668980 +.00000000 +00000-0 +27225-1 0 00002
2 56147 43.0042 34.5944 0001922 245.4323 195.6853 15.47146246 01
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001922 |
| inclination: | 43.0042° |
| perigee height: | 424 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 34.5944° |
| argument of perigee: | 245.4323° |
| revolutions per day: | 15.47146246 |
| mean anomaly at epoch: | 195.6853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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