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 46723U 26145.43784204 +.00000000 +00000-0 +74011-3 0 00001
2 46723 53.0424 162.1165 0007917 48.3580 311.8115 15.74943201 02
| Epoch (UTC): | 25 May 2026 10:30:29 |
| Eccentricity: | 0.0007917 |
| inclination: | 53.0424° |
| perigee height: | 339 km |
| apogee height: | 350 km |
| right ascension of ascending node: | 162.1165° |
| argument of perigee: | 48.3580° |
| revolutions per day: | 15.74943201 |
| mean anomaly at epoch: | 311.8115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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