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 25191.60376892 .00000101 00000-0 44299-4 0 9995
2 21419 74.0409 309.6619 0041071 238.7275 120.9852 14.35085656782382
| Epoch (UTC): | 10 July 2025 14:29:25 |
| Eccentricity: | 0.0041071 |
| inclination: | 74.0409° |
| perigee height: | 745 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 309.6619° |
| argument of perigee: | 238.7275° |
| revolutions per day: | 14.35085656 |
| mean anomaly at epoch: | 120.9852° |
| orbit number at epoch: | 78238 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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