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 56946U 26145.63743852 +.00000000 +00000-0 +21288-3 0 00003
2 56946 97.6211 288.6445 0006873 48.2848 311.8983 15.37964242 09
| Epoch (UTC): | 25 May 2026 15:17:54 |
| Eccentricity: | 0.0006873 |
| inclination: | 97.6211° |
| perigee height: | 447 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 288.6445° |
| argument of perigee: | 48.2848° |
| revolutions per day: | 15.37964242 |
| mean anomaly at epoch: | 311.8983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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