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 data is extracted from the following two-line orbital elements,
1 22276U 92089B 25342.22553448 .00005860 00000-0 46799-3 0 9993
2 22276 20.2828 182.3651 0051184 119.3113 241.2440 14.95166689763072
| Epoch (UTC): | 08 December 2025 05:24:46 |
| Eccentricity: | 0.0051184 |
| inclination: | 20.2828° |
| perigee height: | 546 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 182.3651° |
| argument of perigee: | 119.3113° |
| revolutions per day: | 14.95166689 |
| mean anomaly at epoch: | 241.2440° |
| orbit number at epoch: | 76307 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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