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 63462U 26145.47416088 +.00000000 +00000-0 +43132-3 0 00006
2 63462 43.0003 185.8152 0001465 275.3156 84.7529 15.27589084 02
| Epoch (UTC): | 25 May 2026 11:22:47 |
| Eccentricity: | 0.0001465 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.8152° |
| argument of perigee: | 275.3156° |
| revolutions per day: | 15.27589084 |
| mean anomaly at epoch: | 84.7529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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