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 25407U 98045B 23152.37573299 .00000184 00000-0 11735-3 0 9995
2 25407 71.0096 149.9698 0005960 142.1270 218.0274 14.15916774283794
| Epoch (UTC): | 01 June 2023 09:01:03 |
| Eccentricity: | 0.0005960 |
| inclination: | 71.0096° |
| perigee height: | 835 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 149.9698° |
| argument of perigee: | 142.1270° |
| revolutions per day: | 14.15916774 |
| mean anomaly at epoch: | 218.0274° |
| orbit number at epoch: | 28379 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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