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 23404U 94077A 25080.84769962 .00000385 00000-0 22781-3 0 9995
2 23404 71.0124 118.2404 0015265 170.5765 189.5647 14.13855866564653
| Epoch (UTC): | 21 March 2025 20:20:41 |
| Eccentricity: | 0.0015265 |
| inclination: | 71.0124° |
| perigee height: | 835 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 118.2404° |
| argument of perigee: | 170.5765° |
| revolutions per day: | 14.13855866 |
| mean anomaly at epoch: | 189.5647° |
| orbit number at epoch: | 56465 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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