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 15752U 26159.40654911 +.00000000 +00000-0 +35731-4 0 00009
2 15752 82.9511 48.1201 0024389 15.4510 344.7384 13.73360606 04
| Epoch (UTC): | 08 June 2026 09:45:25 |
| Eccentricity: | 0.0024389 |
| inclination: | 82.9511° |
| perigee height: | 970 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 48.1201° |
| argument of perigee: | 15.4510° |
| revolutions per day: | 13.73360606 |
| mean anomaly at epoch: | 344.7384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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