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 61581U 26145.65488051 +.00000000 +00000-0 +18157-4 0 00005
2 61581 53.1595 277.2005 0001081 93.3753 266.7388 15.69712106 02
| Epoch (UTC): | 25 May 2026 15:43:01 |
| Eccentricity: | 0.0001081 |
| inclination: | 53.1595° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 277.2005° |
| argument of perigee: | 93.3753° |
| revolutions per day: | 15.69712106 |
| mean anomaly at epoch: | 266.7388° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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