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 56885U 26145.33185632 +.00000000 +00000-0 +73728-3 0 00004
2 56885 43.0015 12.2044 0001366 268.2599 91.8096 15.27490955 07
| Epoch (UTC): | 25 May 2026 07:57:52 |
| Eccentricity: | 0.0001366 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 12.2044° |
| argument of perigee: | 268.2599° |
| revolutions per day: | 15.27490955 |
| mean anomaly at epoch: | 91.8096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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