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 25119U 26106.09528257 +.00000000 +00000-0 +21843-3 0 00005
2 25119 45.0149 352.3266 0003262 322.4971 37.5653 14.47406467 03
| Epoch (UTC): | 16 April 2026 02:17:12 |
| Eccentricity: | 0.0003262 |
| inclination: | 45.0149° |
| perigee height: | 732 km |
| apogee height: | 736 km |
| right ascension of ascending node: | 352.3266° |
| argument of perigee: | 322.4971° |
| revolutions per day: | 14.47406467 |
| mean anomaly at epoch: | 37.5653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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