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 10515U 26129.72883586 +.00000000 +00000-0 -90946-5 0 00006
2 10515 81.2470 2.8115 0024505 82.0293 278.3657 14.09114929 01
| Epoch (UTC): | 09 May 2026 17:29:31 |
| Eccentricity: | 0.0024505 |
| inclination: | 81.2470° |
| perigee height: | 845 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 2.8115° |
| argument of perigee: | 82.0293° |
| revolutions per day: | 14.09114929 |
| mean anomaly at epoch: | 278.3657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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