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 61756U 26145.61125734 +.00000000 +00000-0 +71553-3 0 00009
2 61756 97.2942 24.1328 0004049 29.1332 331.0153 15.65352395 07
| Epoch (UTC): | 25 May 2026 14:40:12 |
| Eccentricity: | 0.0004049 |
| inclination: | 97.2942° |
| perigee height: | 369 km |
| apogee height: | 375 km |
| right ascension of ascending node: | 24.1328° |
| argument of perigee: | 29.1332° |
| revolutions per day: | 15.65352395 |
| mean anomaly at epoch: | 331.0153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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