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 25083.18138713 .00000583 00000-0 28671-3 0 9997
2 40069 98.4636 71.2963 0004542 263.9972 96.0688 14.21252426555391
| Epoch (UTC): | 24 March 2025 04:21:11 |
| Eccentricity: | 0.0004542 |
| inclination: | 98.4636° |
| perigee height: | 818 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 71.2963° |
| argument of perigee: | 263.9972° |
| revolutions per day: | 14.21252426 |
| mean anomaly at epoch: | 96.0688° |
| orbit number at epoch: | 55539 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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