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 54194U 26145.62906137 +.00000000 +00000-0 -83820-4 0 00004
2 54194 53.2120 8.6882 0001423 94.1027 266.0128 15.08847225 00
| Epoch (UTC): | 25 May 2026 15:05:50 |
| Eccentricity: | 0.0001423 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 8.6882° |
| argument of perigee: | 94.1027° |
| revolutions per day: | 15.08847225 |
| mean anomaly at epoch: | 266.0128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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