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 26068.63256573 +.00000000 +00000-0 +59657-3 0 00000
2 25114 45.0119 176.5268 0005360 142.0481 218.0749 14.46442017 08
| Epoch (UTC): | 09 March 2026 15:10:53 |
| Eccentricity: | 0.0005360 |
| inclination: | 45.0119° |
| perigee height: | 733 km |
| apogee height: | 741 km |
| right ascension of ascending node: | 176.5268° |
| argument of perigee: | 142.0481° |
| revolutions per day: | 14.46442017 |
| mean anomaly at epoch: | 218.0749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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