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 62061U 26145.16385522 +.00000000 +00000-0 +21803-2 0 00004
2 62061 53.1565 54.3417 0001055 96.6881 263.4257 15.69768548 03
| Epoch (UTC): | 25 May 2026 03:55:57 |
| Eccentricity: | 0.0001055 |
| inclination: | 53.1565° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 54.3417° |
| argument of perigee: | 96.6881° |
| revolutions per day: | 15.69768548 |
| mean anomaly at epoch: | 263.4257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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