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 66199U 26145.55198034 +.00000000 +00000-0 +44888-3 0 00002
2 66199 53.1601 248.0956 0000431 24.4182 335.6839 15.30203095 07
| Epoch (UTC): | 25 May 2026 13:14:51 |
| Eccentricity: | 0.0000431 |
| inclination: | 53.1601° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.0956° |
| argument of perigee: | 24.4182° |
| revolutions per day: | 15.30203095 |
| mean anomaly at epoch: | 335.6839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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