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 40069U 14037A 25119.22604696 .00000270 00000-0 14319-3 0 9997
2 40069 98.4666 105.8594 0006240 148.9856 211.1692 14.21280909560510
| Epoch (UTC): | 29 April 2025 05:25:30 |
| Eccentricity: | 0.0006240 |
| inclination: | 98.4666° |
| perigee height: | 816 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 105.8594° |
| argument of perigee: | 148.9856° |
| revolutions per day: | 14.21280909 |
| mean anomaly at epoch: | 211.1692° |
| orbit number at epoch: | 56051 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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