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 61722U 26145.30716663 +.00000000 +00000-0 +18216-4 0 00003
2 61722 53.1602 105.7033 0001302 86.0159 274.0991 15.30196570 00
| Epoch (UTC): | 25 May 2026 07:22:19 |
| Eccentricity: | 0.0001302 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 105.7033° |
| argument of perigee: | 86.0159° |
| revolutions per day: | 15.30196570 |
| mean anomaly at epoch: | 274.0991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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