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 00046U 26134.91414199 +.00000000 +00000-0 +58954-4 0 00002
2 00046 66.6882 318.9587 0200130 316.7816 41.7735 14.54837574 02
| Epoch (UTC): | 14 May 2026 21:56:21 |
| Eccentricity: | 0.0200130 |
| inclination: | 66.6882° |
| perigee height: | 568 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 318.9587° |
| argument of perigee: | 316.7816° |
| revolutions per day: | 14.54837574 |
| mean anomaly at epoch: | 41.7735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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