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 61211U 26145.27775455 +.00000000 +00000-0 +83237-5 0 00002
2 61211 53.1584 159.0067 0000715 84.2667 275.8432 15.69710703 03
| Epoch (UTC): | 25 May 2026 06:39:57 |
| Eccentricity: | 0.0000715 |
| inclination: | 53.1584° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 159.0067° |
| argument of perigee: | 84.2667° |
| revolutions per day: | 15.69710703 |
| mean anomaly at epoch: | 275.8432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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