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 26132.98925917 +.00000000 +00000-0 +61492-4 0 00003
2 00046 66.6883 324.2067 0199998 318.1918 40.4057 14.54836356 04
| Epoch (UTC): | 12 May 2026 23:44:31 |
| Eccentricity: | 0.0199998 |
| inclination: | 66.6883° |
| perigee height: | 568 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 324.2067° |
| argument of perigee: | 318.1918° |
| revolutions per day: | 14.54836356 |
| mean anomaly at epoch: | 40.4057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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