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 57615U 26145.62589644 +.00000000 +00000-0 +10529-3 0 00009
2 57615 43.0029 6.9879 0001395 262.5150 97.5544 15.27583429 02
| Epoch (UTC): | 25 May 2026 15:01:17 |
| Eccentricity: | 0.0001395 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 6.9879° |
| argument of perigee: | 262.5150° |
| revolutions per day: | 15.27583429 |
| mean anomaly at epoch: | 97.5544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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