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 56548U 26145.48395334 +.00000000 +00000-0 +35596-4 0 00000
2 56548 43.0026 150.1617 0001482 267.6712 92.3971 15.27579638 06
| Epoch (UTC): | 25 May 2026 11:36:53 |
| Eccentricity: | 0.0001482 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 150.1617° |
| argument of perigee: | 267.6712° |
| revolutions per day: | 15.27579638 |
| mean anomaly at epoch: | 92.3971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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