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 63711U 26145.59834900 +.00000000 +00000-0 +39598-3 0 00004
2 63711 53.1592 222.3975 0001000 93.8678 266.2438 15.31714298 09
| Epoch (UTC): | 25 May 2026 14:21:37 |
| Eccentricity: | 0.0001000 |
| inclination: | 53.1592° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 222.3975° |
| argument of perigee: | 93.8678° |
| revolutions per day: | 15.31714298 |
| mean anomaly at epoch: | 266.2438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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