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 56705U 26145.46345098 +.00000000 +00000-0 +21082-4 0 00000
2 56705 43.0007 189.4781 0001505 274.5342 85.5338 15.27576528 05
| Epoch (UTC): | 25 May 2026 11:07:22 |
| Eccentricity: | 0.0001505 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.4781° |
| argument of perigee: | 274.5342° |
| revolutions per day: | 15.27576528 |
| mean anomaly at epoch: | 85.5338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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