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 40071U 14037C 25109.25301729 .00003074 00000-0 34217-3 0 9997
2 40071 98.3417 42.3903 0006690 200.0546 160.0407 14.87905639583102
| Epoch (UTC): | 19 April 2025 06:04:20 |
| Eccentricity: | 0.0006690 |
| inclination: | 98.3417° |
| perigee height: | 600 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 42.3903° |
| argument of perigee: | 200.0546° |
| revolutions per day: | 14.87905639 |
| mean anomaly at epoch: | 160.0407° |
| orbit number at epoch: | 58310 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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