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 26150.40541549 +.00000000 +00000-0 +45069-3 0 00004
2 25119 45.0120 139.0467 0002610 230.6647 129.3974 14.47514824 04
| Epoch (UTC): | 30 May 2026 09:43:47 |
| Eccentricity: | 0.0002610 |
| inclination: | 45.0120° |
| perigee height: | 732 km |
| apogee height: | 736 km |
| right ascension of ascending node: | 139.0467° |
| argument of perigee: | 230.6647° |
| revolutions per day: | 14.47514824 |
| mean anomaly at epoch: | 129.3974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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