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 14781U 84021B 25342.16005478 .00002215 00000-0 23463-3 0 9994
2 14781 97.7809 305.2596 0009240 94.7136 265.5137 14.90116000228674
| Epoch (UTC): | 08 December 2025 03:50:28 |
| Eccentricity: | 0.0009240 |
| inclination: | 97.7809° |
| perigee height: | 591 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 305.2596° |
| argument of perigee: | 94.7136° |
| revolutions per day: | 14.90116000 |
| mean anomaly at epoch: | 265.5137° |
| orbit number at epoch: | 22867 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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