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 57014U 26145.60115179 +.00000000 +00000-0 +42988-3 0 00002
2 57014 97.4938 256.1446 0006195 121.3874 238.7973 15.31087242 06
| Epoch (UTC): | 25 May 2026 14:25:39 |
| Eccentricity: | 0.0006195 |
| inclination: | 97.4938° |
| perigee height: | 468 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 256.1446° |
| argument of perigee: | 121.3874° |
| revolutions per day: | 15.31087242 |
| mean anomaly at epoch: | 238.7973° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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