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 25194.19170009 .00000964 00000-0 10707-3 0 9991
2 14781 97.7562 159.9005 0006752 216.7970 143.2785 14.89463054227645
| Epoch (UTC): | 13 July 2025 04:36:02 |
| Eccentricity: | 0.0006752 |
| inclination: | 97.7562° |
| perigee height: | 595 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 159.9005° |
| argument of perigee: | 216.7970° |
| revolutions per day: | 14.89463054 |
| mean anomaly at epoch: | 143.2785° |
| orbit number at epoch: | 22764 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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