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 15159U 26150.40883911 +.00000000 +00000-0 +00000-0 0 00002
2 15159 12.7787 334.0800 0035984 54.1532 160.9458 0.98397586 00
| Epoch (UTC): | 30 May 2026 09:48:43 |
| Eccentricity: | 0.0035984 |
| inclination: | 12.7787° |
| perigee height: | 36167 km |
| apogee height: | 36474 km |
| right ascension of ascending node: | 334.0800° |
| argument of perigee: | 54.1532° |
| revolutions per day: | 0.98397586 |
| mean anomaly at epoch: | 160.9458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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