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 27421U 02021A 25200.15765806 .00000249 00000-0 63265-4 0 9999
2 27421 98.0334 247.9718 0129366 231.2119 127.7466 14.54325814214466
| Epoch (UTC): | 19 July 2025 03:47:01 |
| Eccentricity: | 0.0129366 |
| inclination: | 98.0334° |
| perigee height: | 620 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 247.9718° |
| argument of perigee: | 231.2119° |
| revolutions per day: | 14.54325814 |
| mean anomaly at epoch: | 127.7466° |
| orbit number at epoch: | 21446 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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