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 46705U 26144.64107594 +.00000000 +00000-0 +55948-3 0 00002
2 46705 53.0445 233.8717 0002387 333.7246 26.3648 15.66134546 04
| Epoch (UTC): | 24 May 2026 15:23:08 |
| Eccentricity: | 0.0002387 |
| inclination: | 53.0445° |
| perigee height: | 368 km |
| apogee height: | 372 km |
| right ascension of ascending node: | 233.8717° |
| argument of perigee: | 333.7246° |
| revolutions per day: | 15.66134546 |
| mean anomaly at epoch: | 26.3648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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