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 57051U 26145.05044347 +.00000000 +00000-0 -75813-5 0 00006
2 57051 43.0050 39.1763 0001379 250.6054 109.4648 15.27580503 01
| Epoch (UTC): | 25 May 2026 01:12:38 |
| Eccentricity: | 0.0001379 |
| inclination: | 43.0050° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 39.1763° |
| argument of perigee: | 250.6054° |
| revolutions per day: | 15.27580503 |
| mean anomaly at epoch: | 109.4648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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