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 61864U 26145.51545462 +.00000000 +00000-0 +34587-4 0 00009
2 61864 43.0034 164.4206 0001667 275.9931 84.0730 15.27578146 08
| Epoch (UTC): | 25 May 2026 12:22:15 |
| Eccentricity: | 0.0001667 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.4206° |
| argument of perigee: | 275.9931° |
| revolutions per day: | 15.27578146 |
| mean anomaly at epoch: | 84.0730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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