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 61255U 26145.40016822 +.00000000 +00000-0 +73113-5 0 00003
2 61255 53.1595 38.1842 0000845 120.7039 239.4062 15.69708482 00
| Epoch (UTC): | 25 May 2026 09:36:14 |
| Eccentricity: | 0.0000845 |
| inclination: | 53.1595° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 38.1842° |
| argument of perigee: | 120.7039° |
| revolutions per day: | 15.69708482 |
| mean anomaly at epoch: | 239.4062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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