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 61890U 26145.34686913 +.00000000 +00000-0 -81690-5 0 00005
2 61890 53.1623 130.3412 0001128 95.0748 265.0384 15.34398802 06
| Epoch (UTC): | 25 May 2026 08:19:29 |
| Eccentricity: | 0.0001128 |
| inclination: | 53.1623° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 130.3412° |
| argument of perigee: | 95.0748° |
| revolutions per day: | 15.34398802 |
| mean anomaly at epoch: | 265.0384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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