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 56961U 26145.40055457 +.00000000 +00000-0 +14218-2 0 00006
2 56961 97.5640 308.8898 0010391 278.0813 81.9289 16.05636318 03
| Epoch (UTC): | 25 May 2026 09:36:47 |
| Eccentricity: | 0.0010391 |
| inclination: | 97.5640° |
| perigee height: | 252 km |
| apogee height: | 266 km |
| right ascension of ascending node: | 308.8898° |
| argument of perigee: | 278.0813° |
| revolutions per day: | 16.05636318 |
| mean anomaly at epoch: | 81.9289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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