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 25114U 26105.92751663 +.00000000 +00000-0 +20604-3 0 00004
2 25114 45.0151 357.2928 0005904 319.7680 40.2735 14.46559047 05
| Epoch (UTC): | 15 April 2026 22:15:37 |
| Eccentricity: | 0.0005904 |
| inclination: | 45.0151° |
| perigee height: | 733 km |
| apogee height: | 741 km |
| right ascension of ascending node: | 357.2928° |
| argument of perigee: | 319.7680° |
| revolutions per day: | 14.46559047 |
| mean anomaly at epoch: | 40.2735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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