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 56835U 26145.36857995 +.00000000 +00000-0 +16325-2 0 00009
2 56835 42.9939 28.1054 0010810 233.3755 126.6106 15.35655755 02
| Epoch (UTC): | 25 May 2026 08:50:45 |
| Eccentricity: | 0.0010810 |
| inclination: | 42.9939° |
| perigee height: | 452 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 28.1054° |
| argument of perigee: | 233.3755° |
| revolutions per day: | 15.35655755 |
| mean anomaly at epoch: | 126.6106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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