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 61865U 26145.45392319 +.00000000 +00000-0 +99397-4 0 00004
2 61865 43.0006 164.8156 0001486 268.8409 91.2272 15.27584759 04
| Epoch (UTC): | 25 May 2026 10:53:38 |
| Eccentricity: | 0.0001486 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.8156° |
| argument of perigee: | 268.8409° |
| revolutions per day: | 15.27584759 |
| mean anomaly at epoch: | 91.2272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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