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 57145U 26145.59685522 +.00000000 +00000-0 +10426-4 0 00002
2 57145 43.0013 189.1465 0001065 275.8648 84.2083 15.27576300 02
| Epoch (UTC): | 25 May 2026 14:19:28 |
| Eccentricity: | 0.0001065 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.1465° |
| argument of perigee: | 275.8648° |
| revolutions per day: | 15.27576300 |
| mean anomaly at epoch: | 84.2083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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