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 61861U 26145.50132564 +.00000000 +00000-0 -60288-4 0 00008
2 61861 43.0021 164.3160 0000996 303.6266 56.4490 15.27572754 08
| Epoch (UTC): | 25 May 2026 12:01:54 |
| Eccentricity: | 0.0000996 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.3160° |
| argument of perigee: | 303.6266° |
| revolutions per day: | 15.27572754 |
| mean anomaly at epoch: | 56.4490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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