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 61563U 26145.58675306 +.00000000 +00000-0 +20620-3 0 00005
2 61563 88.9832 63.9510 0005571 292.9125 67.1438 13.50046182 02
| Epoch (UTC): | 25 May 2026 14:04:55 |
| Eccentricity: | 0.0005571 |
| inclination: | 88.9832° |
| perigee height: | 1068 km |
| apogee height: | 1076 km |
| right ascension of ascending node: | 63.9510° |
| argument of perigee: | 292.9125° |
| revolutions per day: | 13.50046182 |
| mean anomaly at epoch: | 67.1438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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