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 61190U 26145.61257451 +.00000000 +00000-0 +20926-3 0 00001
2 61190 97.5554 234.8705 0008048 94.1795 266.0353 15.08654990 00
| Epoch (UTC): | 25 May 2026 14:42:06 |
| Eccentricity: | 0.0008048 |
| inclination: | 97.5554° |
| perigee height: | 535 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 234.8705° |
| argument of perigee: | 94.1795° |
| revolutions per day: | 15.08654990 |
| mean anomaly at epoch: | 266.0353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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