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 61557U 26145.55946919 +.00000000 +00000-0 +22940-3 0 00003
2 61557 88.9827 58.0281 0011126 115.7347 244.4995 14.24043177 01
| Epoch (UTC): | 25 May 2026 13:25:38 |
| Eccentricity: | 0.0011126 |
| inclination: | 88.9827° |
| perigee height: | 804 km |
| apogee height: | 820 km |
| right ascension of ascending node: | 58.0281° |
| argument of perigee: | 115.7347° |
| revolutions per day: | 14.24043177 |
| mean anomaly at epoch: | 244.4995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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