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 57137U 26145.42882487 +.00000000 +00000-0 +62241-5 0 00007
2 57137 43.0031 189.6220 0001005 279.9825 80.0913 15.27574337 07
| Epoch (UTC): | 25 May 2026 10:17:30 |
| Eccentricity: | 0.0001005 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.6220° |
| argument of perigee: | 279.9825° |
| revolutions per day: | 15.27574337 |
| mean anomaly at epoch: | 80.0913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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