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 61941U 26145.60948293 +.00000000 +00000-0 +23131-2 0 00005
2 61941 53.1571 351.7384 0000119 210.3993 149.7018 15.69872565 08
| Epoch (UTC): | 25 May 2026 14:37:39 |
| Eccentricity: | 0.0000119 |
| inclination: | 53.1571° |
| perigee height: | 359 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 351.7384° |
| argument of perigee: | 210.3993° |
| revolutions per day: | 15.69872565 |
| mean anomaly at epoch: | 149.7018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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