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 61668U 26145.55579229 +.00000000 +00000-0 +22440-4 0 00008
2 61668 53.1616 94.0817 0001355 92.3673 267.7483 15.30195005 00
| Epoch (UTC): | 25 May 2026 13:20:20 |
| Eccentricity: | 0.0001355 |
| inclination: | 53.1616° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 94.0817° |
| argument of perigee: | 92.3673° |
| revolutions per day: | 15.30195005 |
| mean anomaly at epoch: | 267.7483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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