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 61780U 26145.61129720 +.00000000 +00000-0 +64896-3 0 00007
2 61780 97.2969 21.1931 0007772 29.2818 330.8871 15.56678439 00
| Epoch (UTC): | 25 May 2026 14:40:16 |
| Eccentricity: | 0.0007772 |
| inclination: | 97.2969° |
| perigee height: | 392 km |
| apogee height: | 403 km |
| right ascension of ascending node: | 21.1931° |
| argument of perigee: | 29.2818° |
| revolutions per day: | 15.56678439 |
| mean anomaly at epoch: | 330.8871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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