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 66289U 26145.33471552 +.00000000 +00000-0 +44599-3 0 00006
2 66289 53.1594 194.3473 0000634 90.5044 269.6031 15.34389115 03
| Epoch (UTC): | 25 May 2026 08:01:59 |
| Eccentricity: | 0.0000634 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 194.3473° |
| argument of perigee: | 90.5044° |
| revolutions per day: | 15.34389115 |
| mean anomaly at epoch: | 269.6031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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