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 57451U 26145.56262953 +.00000000 +00000-0 +23751-3 0 00002
2 57451 43.0038 185.2862 0001638 297.0692 62.9992 15.27575298 05
| Epoch (UTC): | 25 May 2026 13:30:11 |
| Eccentricity: | 0.0001638 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.2862° |
| argument of perigee: | 297.0692° |
| revolutions per day: | 15.27575298 |
| mean anomaly at epoch: | 62.9992° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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