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 63471U 26145.58323801 +.00000000 +00000-0 +57296-3 0 00004
2 63471 43.0006 185.7725 0001746 271.4468 88.6184 15.27592876 08
| Epoch (UTC): | 25 May 2026 13:59:51 |
| Eccentricity: | 0.0001746 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.7725° |
| argument of perigee: | 271.4468° |
| revolutions per day: | 15.27592876 |
| mean anomaly at epoch: | 88.6184° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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