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 63477U 26145.55803503 +.00000000 +00000-0 +19515-3 0 00001
2 63477 43.0020 182.1071 0001889 257.1798 102.8843 15.27548009 00
| Epoch (UTC): | 25 May 2026 13:23:34 |
| Eccentricity: | 0.0001889 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 182.1071° |
| argument of perigee: | 257.1798° |
| revolutions per day: | 15.27548009 |
| mean anomaly at epoch: | 102.8843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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