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 12792U 26088.14526191 +.00000000 +00000-0 +90745-4 0 00006
2 12792 74.0276 247.7844 0012593 116.4502 243.7946 14.39017053 02
| Epoch (UTC): | 29 March 2026 03:29:10 |
| Eccentricity: | 0.0012593 |
| inclination: | 74.0276° |
| perigee height: | 753 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 247.7844° |
| argument of perigee: | 116.4502° |
| revolutions per day: | 14.39017053 |
| mean anomaly at epoch: | 243.7946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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