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 65886U 26145.06499166 +.00000000 +00000-0 +73913-3 0 00001
2 65886 53.1593 15.4644 0000966 84.9512 275.1601 15.34403273 09
| Epoch (UTC): | 25 May 2026 01:33:35 |
| Eccentricity: | 0.0000966 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 15.4644° |
| argument of perigee: | 84.9512° |
| revolutions per day: | 15.34403273 |
| mean anomaly at epoch: | 275.1601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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