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 22915U 26139.68309955 +.00000000 +00000-0 +00000-0 0 00008
2 22915 13.7664 15.6724 0006534 10.7585 182.1726 0.98531793 09
| Epoch (UTC): | 19 May 2026 16:23:39 |
| Eccentricity: | 0.0006534 |
| inclination: | 13.7664° |
| perigee height: | 36254 km |
| apogee height: | 36309 km |
| right ascension of ascending node: | 15.6724° |
| argument of perigee: | 10.7585° |
| revolutions per day: | 0.98531793 |
| mean anomaly at epoch: | 182.1726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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