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 61944U 26145.59486832 +.00000000 +00000-0 +23178-2 0 00003
2 61944 53.1567 352.3727 0000413 143.8915 216.2131 15.69878517 04
| Epoch (UTC): | 25 May 2026 14:16:36 |
| Eccentricity: | 0.0000413 |
| inclination: | 53.1567° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 352.3727° |
| argument of perigee: | 143.8915° |
| revolutions per day: | 15.69878517 |
| mean anomaly at epoch: | 216.2131° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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