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 61196U 26145.57369941 +.00000000 +00000-0 +12631-3 0 00004
2 61196 44.8580 237.8089 0007179 343.8165 16.2435 13.99138960 05
| Epoch (UTC): | 25 May 2026 13:46:07 |
| Eccentricity: | 0.0007179 |
| inclination: | 44.8580° |
| perigee height: | 892 km |
| apogee height: | 902 km |
| right ascension of ascending node: | 237.8089° |
| argument of perigee: | 343.8165° |
| revolutions per day: | 13.99138960 |
| mean anomaly at epoch: | 16.2435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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