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 66281U 26145.38908519 +.00000000 +00000-0 +36067-3 0 00002
2 66281 53.1591 195.3955 0001031 90.8336 269.2783 15.30198838 03
| Epoch (UTC): | 25 May 2026 09:20:16 |
| Eccentricity: | 0.0001031 |
| inclination: | 53.1591° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 195.3955° |
| argument of perigee: | 90.8336° |
| revolutions per day: | 15.30198838 |
| mean anomaly at epoch: | 269.2783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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