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 66284U 26145.50705050 +.00000000 +00000-0 +35625-3 0 00003
2 66284 53.1578 194.7094 0001122 89.0449 271.0680 15.30203888 03
| Epoch (UTC): | 25 May 2026 12:10:09 |
| Eccentricity: | 0.0001122 |
| inclination: | 53.1578° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 194.7094° |
| argument of perigee: | 89.0449° |
| revolutions per day: | 15.30203888 |
| mean anomaly at epoch: | 271.0680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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