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 57053U 26145.40692689 +.00000000 +00000-0 +62975-6 0 00000
2 57053 43.0038 37.5473 0001142 272.6101 87.4620 15.27576701 04
| Epoch (UTC): | 25 May 2026 09:45:58 |
| Eccentricity: | 0.0001142 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 37.5473° |
| argument of perigee: | 272.6101° |
| revolutions per day: | 15.27576701 |
| mean anomaly at epoch: | 87.4620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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