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 56833U 26145.31111823 +.00000000 +00000-0 +95942-3 0 00008
2 56833 43.0040 11.7461 0003150 234.1424 125.9134 15.23258245 09
| Epoch (UTC): | 25 May 2026 07:28:00 |
| Eccentricity: | 0.0003150 |
| inclination: | 43.0040° |
| perigee height: | 494 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 11.7461° |
| argument of perigee: | 234.1424° |
| revolutions per day: | 15.23258245 |
| mean anomaly at epoch: | 125.9134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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