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 65984U 26145.49790078 +.00000000 +00000-0 -40298-2 0 00003
2 65984 81.3012 232.6947 0000885 234.5705 125.5368 13.83823242 05
| Epoch (UTC): | 25 May 2026 11:56:58 |
| Eccentricity: | 0.0000885 |
| inclination: | 81.3012° |
| perigee height: | 950 km |
| apogee height: | 951 km |
| right ascension of ascending node: | 232.6947° |
| argument of perigee: | 234.5705° |
| revolutions per day: | 13.83823242 |
| mean anomaly at epoch: | 125.5368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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