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 65048U 26145.57050334 +.00000000 +00000-0 +67437-4 0 00002
2 65048 50.0060 346.8147 0000467 42.0842 318.0066 13.29323592 09
| Epoch (UTC): | 25 May 2026 13:41:31 |
| Eccentricity: | 0.0000467 |
| inclination: | 50.0060° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 346.8147° |
| argument of perigee: | 42.0842° |
| revolutions per day: | 13.29323592 |
| mean anomaly at epoch: | 318.0066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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