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 21419U 91041B 25188.60622196 .00000127 00000-0 53404-4 0 9998
2 21419 74.0408 315.1552 0041104 244.7852 114.9036 14.35084805781958
| Epoch (UTC): | 07 July 2025 14:32:57 |
| Eccentricity: | 0.0041104 |
| inclination: | 74.0408° |
| perigee height: | 745 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 315.1552° |
| argument of perigee: | 244.7852° |
| revolutions per day: | 14.35084805 |
| mean anomaly at epoch: | 114.9036° |
| orbit number at epoch: | 78195 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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