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 57193U 26145.61552942 +.00000000 +00000-0 +44429-3 0 00006
2 57193 97.5070 210.8076 0011214 170.3059 189.8400 15.31421182 01
| Epoch (UTC): | 25 May 2026 14:46:21 |
| Eccentricity: | 0.0011214 |
| inclination: | 97.5070° |
| perigee height: | 464 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 210.8076° |
| argument of perigee: | 170.3059° |
| revolutions per day: | 15.31421182 |
| mean anomaly at epoch: | 189.8400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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