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 65689U 26145.58335992 +.00000000 +00000-0 +66286-3 0 00000
2 65689 53.1570 348.6943 0000779 351.8449 8.2539 15.30211119 02
| Epoch (UTC): | 25 May 2026 14:00:02 |
| Eccentricity: | 0.0000779 |
| inclination: | 53.1570° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 348.6943° |
| argument of perigee: | 351.8449° |
| revolutions per day: | 15.30211119 |
| mean anomaly at epoch: | 8.2539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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