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 25109.22934997 .00000284 00000-0 14938-3 0 9998
2 40069 98.4660 96.2718 0005643 176.3926 183.7293 14.21274113559096
| Epoch (UTC): | 19 April 2025 05:30:15 |
| Eccentricity: | 0.0005643 |
| inclination: | 98.4660° |
| perigee height: | 817 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 96.2718° |
| argument of perigee: | 176.3926° |
| revolutions per day: | 14.21274113 |
| mean anomaly at epoch: | 183.7293° |
| orbit number at epoch: | 55909 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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