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 26158.91229712 +.00000000 +00000-0 -51614-4 0 00002
2 10515 81.2437 334.4472 0022470 359.2717 0.8417 14.09112362 04
| Epoch (UTC): | 07 June 2026 21:53:42 |
| Eccentricity: | 0.0022470 |
| inclination: | 81.2437° |
| perigee height: | 846 km |
| apogee height: | 879 km |
| right ascension of ascending node: | 334.4472° |
| argument of perigee: | 359.2717° |
| revolutions per day: | 14.09112362 |
| mean anomaly at epoch: | 0.8417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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