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 53194U 26145.57697476 +.00000000 +00000-0 -82855-3 0 00006
2 53194 97.4490 206.5885 0001994 144.9547 215.1812 15.05710222 03
| Epoch (UTC): | 25 May 2026 13:50:50 |
| Eccentricity: | 0.0001994 |
| inclination: | 97.4490° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 206.5885° |
| argument of perigee: | 144.9547° |
| revolutions per day: | 15.05710222 |
| mean anomaly at epoch: | 215.1812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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