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 57181U 26145.56381969 +.00000000 +00000-0 +17924-3 0 00006
2 57181 97.5081 199.8146 0014360 210.2160 149.8245 15.14329897 00
| Epoch (UTC): | 25 May 2026 13:31:54 |
| Eccentricity: | 0.0014360 |
| inclination: | 97.5081° |
| perigee height: | 513 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 199.8146° |
| argument of perigee: | 210.2160° |
| revolutions per day: | 15.14329897 |
| mean anomaly at epoch: | 149.8245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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