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 57194U 26145.55133727 +.00000000 +00000-0 +36265-3 0 00005
2 57194 97.5079 208.3179 0011867 179.0982 181.0279 15.25128376 02
| Epoch (UTC): | 25 May 2026 13:13:55 |
| Eccentricity: | 0.0011867 |
| inclination: | 97.5079° |
| perigee height: | 482 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 208.3179° |
| argument of perigee: | 179.0982° |
| revolutions per day: | 15.25128376 |
| mean anomaly at epoch: | 181.0279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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