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 61045U 26145.01888323 +.00000000 +00000-0 -18664-2 0 00008
2 61045 52.9714 55.9758 0006583 54.6325 305.5284 15.20684254 06
| Epoch (UTC): | 25 May 2026 00:27:11 |
| Eccentricity: | 0.0006583 |
| inclination: | 52.9714° |
| perigee height: | 499 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 55.9758° |
| argument of perigee: | 54.6325° |
| revolutions per day: | 15.20684254 |
| mean anomaly at epoch: | 305.5284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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