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 26083.49081266 +.00000000 +00000-0 +21461-3 0 00005
2 00046 66.6864 99.1395 0196130 354.7907 5.1157 14.54715537 00
| Epoch (UTC): | 24 March 2026 11:46:46 |
| Eccentricity: | 0.0196130 |
| inclination: | 66.6864° |
| perigee height: | 571 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 99.1395° |
| argument of perigee: | 354.7907° |
| revolutions per day: | 14.54715537 |
| mean anomaly at epoch: | 5.1157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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