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 40025U 14033R 25193.92504696 .00005507 00000-0 33471-3 0 9991
2 40025 98.0839 178.3834 0008719 308.0872 51.9569 15.10896745601678
| Epoch (UTC): | 12 July 2025 22:12:04 |
| Eccentricity: | 0.0008719 |
| inclination: | 98.0839° |
| perigee height: | 527 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 178.3834° |
| argument of perigee: | 308.0872° |
| revolutions per day: | 15.10896745 |
| mean anomaly at epoch: | 51.9569° |
| orbit number at epoch: | 60167 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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