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 61191U 26145.62297287 +.00000000 +00000-0 +17951-3 0 00008
2 61191 97.5552 235.3128 0014247 32.0250 328.1841 15.08710423 05
| Epoch (UTC): | 25 May 2026 14:57:04 |
| Eccentricity: | 0.0014247 |
| inclination: | 97.5552° |
| perigee height: | 530 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 235.3128° |
| argument of perigee: | 32.0250° |
| revolutions per day: | 15.08710423 |
| mean anomaly at epoch: | 328.1841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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