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 57221U 26145.66668980 +.00000000 +00000-0 +20259-1 0 00006
2 57221 42.9999 317.8904 0001809 257.8772 171.4084 15.50980815 06
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001809 |
| inclination: | 42.9999° |
| perigee height: | 413 km |
| apogee height: | 415 km |
| right ascension of ascending node: | 317.8904° |
| argument of perigee: | 257.8772° |
| revolutions per day: | 15.50980815 |
| mean anomaly at epoch: | 171.4084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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