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 23276.21868361 -.00000169 00000-0 -61604-4 0 9998
2 25407 71.0095 249.6454 0009733 293.0402 66.9695 14.15936996301590
| Epoch (UTC): | 03 October 2023 05:14:54 |
| Eccentricity: | 0.0009733 |
| inclination: | 71.0095° |
| perigee height: | 832 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 249.6454° |
| argument of perigee: | 293.0402° |
| revolutions per day: | 14.15936996 |
| mean anomaly at epoch: | 66.9695° |
| orbit number at epoch: | 30159 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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