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 65889U 26145.06302876 +.00000000 +00000-0 +10225-2 0 00001
2 65889 53.1584 16.8672 0001125 96.1452 263.9677 15.30212991 03
| Epoch (UTC): | 25 May 2026 01:30:45 |
| Eccentricity: | 0.0001125 |
| inclination: | 53.1584° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 16.8672° |
| argument of perigee: | 96.1452° |
| revolutions per day: | 15.30212991 |
| mean anomaly at epoch: | 263.9677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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