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 07364U 74052B 25080.55502482 .00000107 00000-0 56221-4 0 9992
2 07364 81.2284 283.2295 0051128 98.8539 261.8424 14.06367042599448
| Epoch (UTC): | 21 March 2025 13:19:14 |
| Eccentricity: | 0.0051128 |
| inclination: | 81.2284° |
| perigee height: | 835 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 283.2295° |
| argument of perigee: | 98.8539° |
| revolutions per day: | 14.06367042 |
| mean anomaly at epoch: | 261.8424° |
| orbit number at epoch: | 59944 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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