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 26160.19040573 +.00000000 +00000-0 -54661-4 0 00006
2 10515 81.2437 333.2048 0022382 355.6368 4.4603 14.09112097 06
| Epoch (UTC): | 09 June 2026 04:34:11 |
| Eccentricity: | 0.0022382 |
| inclination: | 81.2437° |
| perigee height: | 846 km |
| apogee height: | 879 km |
| right ascension of ascending node: | 333.2048° |
| argument of perigee: | 355.6368° |
| revolutions per day: | 14.09112097 |
| mean anomaly at epoch: | 4.4603° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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