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 65313U 26145.65032788 +.00000000 +00000-0 +68137-4 0 00007
2 65313 50.0076 286.6735 0000604 97.9981 262.0960 13.29323949 08
| Epoch (UTC): | 25 May 2026 15:36:28 |
| Eccentricity: | 0.0000604 |
| inclination: | 50.0076° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 286.6735° |
| argument of perigee: | 97.9981° |
| revolutions per day: | 13.29323949 |
| mean anomaly at epoch: | 262.0960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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