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 is defined by the following mean orbital elements,
1 25919U 26017.90046117 +.00000000 +00000-0 +16480-3 0 00005
2 25919 98.1556 260.5872 0006290 356.0784 4.0386 14.96673535 02
| Epoch (UTC): | 17 January 2026 21:36:39 |
| Eccentricity: | 0.0006290 |
| inclination: | 98.1556° |
| perigee height: | 573 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 260.5872° |
| argument of perigee: | 356.0784° |
| revolutions per day: | 14.96673535 |
| mean anomaly at epoch: | 4.0386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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