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 18961U 26129.81483520 +.00000000 +00000-0 +23097-3 0 00003
2 18961 98.8728 185.9899 0053806 278.7249 194.6711 14.00735692 05
| Epoch (UTC): | 09 May 2026 19:33:21 |
| Eccentricity: | 0.0053806 |
| inclination: | 98.8728° |
| perigee height: | 852 km |
| apogee height: | 930 km |
| right ascension of ascending node: | 185.9899° |
| argument of perigee: | 278.7249° |
| revolutions per day: | 14.00735692 |
| mean anomaly at epoch: | 194.6711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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