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 61973U 26145.38541885 +.00000000 +00000-0 +55363-3 0 00004
2 61973 42.9979 106.3377 0000967 261.9956 98.0786 15.27594702 05
| Epoch (UTC): | 25 May 2026 09:15:00 |
| Eccentricity: | 0.0000967 |
| inclination: | 42.9979° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 106.3377° |
| argument of perigee: | 261.9956° |
| revolutions per day: | 15.27594702 |
| mean anomaly at epoch: | 98.0786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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