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 61781U 26145.61701449 +.00000000 +00000-0 +21463-3 0 00005
2 61781 97.3036 14.4937 0014912 36.4785 323.7471 15.35294464 01
| Epoch (UTC): | 25 May 2026 14:48:30 |
| Eccentricity: | 0.0014912 |
| inclination: | 97.3036° |
| perigee height: | 450 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 14.4937° |
| argument of perigee: | 36.4785° |
| revolutions per day: | 15.35294464 |
| mean anomaly at epoch: | 323.7471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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