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 57138U 26145.44167564 +.00000000 +00000-0 +18242-5 0 00004
2 57138 43.0023 189.7202 0001323 281.6791 78.3913 15.27574934 08
| Epoch (UTC): | 25 May 2026 10:36:00 |
| Eccentricity: | 0.0001323 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.7202° |
| argument of perigee: | 281.6791° |
| revolutions per day: | 15.27574934 |
| mean anomaly at epoch: | 78.3913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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