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 57527U 26145.41797027 +.00000000 +00000-0 +53720-4 0 00005
2 57527 43.0014 288.4668 0000888 285.3776 74.6977 15.27581144 02
| Epoch (UTC): | 25 May 2026 10:01:52 |
| Eccentricity: | 0.0000888 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 288.4668° |
| argument of perigee: | 285.3776° |
| revolutions per day: | 15.27581144 |
| mean anomaly at epoch: | 74.6977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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