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 65138U 26145.36299337 +.00000000 +00000-0 +30563-3 0 00006
2 65138 51.9004 174.0399 0000572 52.6847 307.4168 14.79946265 05
| Epoch (UTC): | 25 May 2026 08:42:42 |
| Eccentricity: | 0.0000572 |
| inclination: | 51.9004° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 174.0399° |
| argument of perigee: | 52.6847° |
| revolutions per day: | 14.79946265 |
| mean anomaly at epoch: | 307.4168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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