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 57219U 26145.50099890 +.00000000 +00000-0 -13598-4 0 00006
2 57219 43.0020 320.2634 0001349 270.3056 89.7641 15.27582831 02
| Epoch (UTC): | 25 May 2026 12:01:26 |
| Eccentricity: | 0.0001349 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.2634° |
| argument of perigee: | 270.3056° |
| revolutions per day: | 15.27582831 |
| mean anomaly at epoch: | 89.7641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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