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 61063U 26145.13387382 +.00000000 +00000-0 +73381-4 0 00008
2 61063 53.1614 95.8936 0001141 83.8631 276.2500 15.31696929 07
| Epoch (UTC): | 25 May 2026 03:12:46 |
| Eccentricity: | 0.0001141 |
| inclination: | 53.1614° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 95.8936° |
| argument of perigee: | 83.8631° |
| revolutions per day: | 15.31696929 |
| mean anomaly at epoch: | 276.2500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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