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 65990U 26145.53770486 +.00000000 +00000-0 +73890-4 0 00001
2 65990 81.3017 232.5936 0002952 251.4249 108.6587 13.85227105 05
| Epoch (UTC): | 25 May 2026 12:54:17 |
| Eccentricity: | 0.0002952 |
| inclination: | 81.3017° |
| perigee height: | 943 km |
| apogee height: | 948 km |
| right ascension of ascending node: | 232.5936° |
| argument of perigee: | 251.4249° |
| revolutions per day: | 13.85227105 |
| mean anomaly at epoch: | 108.6587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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