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 56163U 26145.36674819 +.00000000 +00000-0 +71858-4 0 00009
2 56163 81.0001 93.4503 0007140 29.5570 330.5988 13.84980259 02
| Epoch (UTC): | 25 May 2026 08:48:07 |
| Eccentricity: | 0.0007140 |
| inclination: | 81.0001° |
| perigee height: | 941 km |
| apogee height: | 952 km |
| right ascension of ascending node: | 93.4503° |
| argument of perigee: | 29.5570° |
| revolutions per day: | 13.84980259 |
| mean anomaly at epoch: | 330.5988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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