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 46727U 26131.26955656 +.00000000 +00000-0 +50178-3 0 00000
2 46727 53.0379 237.6674 0005377 299.9873 60.0608 15.67324368 04
| Epoch (UTC): | 11 May 2026 06:28:09 |
| Eccentricity: | 0.0005377 |
| inclination: | 53.0379° |
| perigee height: | 363 km |
| apogee height: | 370 km |
| right ascension of ascending node: | 237.6674° |
| argument of perigee: | 299.9873° |
| revolutions per day: | 15.67324368 |
| mean anomaly at epoch: | 60.0608° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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