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 61951U 26144.99731791 +.00000000 +00000-0 +14080-2 0 00003
2 61951 53.1573 355.0338 0000818 79.8279 280.2831 15.69769488 01
| Epoch (UTC): | 24 May 2026 23:56:08 |
| Eccentricity: | 0.0000818 |
| inclination: | 53.1573° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 355.0338° |
| argument of perigee: | 79.8279° |
| revolutions per day: | 15.69769488 |
| mean anomaly at epoch: | 280.2831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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