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 65135U 26145.45884565 +.00000000 +00000-0 +28902-3 0 00000
2 65135 51.8978 178.6030 0000386 77.3115 282.7891 14.79931831 09
| Epoch (UTC): | 25 May 2026 11:00:44 |
| Eccentricity: | 0.0000386 |
| inclination: | 51.8978° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 178.6030° |
| argument of perigee: | 77.3115° |
| revolutions per day: | 14.79931831 |
| mean anomaly at epoch: | 282.7891° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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