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 61847U 26145.48849000 +.00000000 +00000-0 +46500-4 0 00009
2 61847 43.0016 152.9700 0001510 270.8286 89.2392 15.27579854 02
| Epoch (UTC): | 25 May 2026 11:43:25 |
| Eccentricity: | 0.0001510 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 152.9700° |
| argument of perigee: | 270.8286° |
| revolutions per day: | 15.27579854 |
| mean anomaly at epoch: | 89.2392° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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