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 47306U 26144.59172998 +.00000000 +00000-0 +00000-0 0 00000
2 47306 0.0273 72.2208 0000090 271.0108 142.9093 1.00272065 04
| Epoch (UTC): | 24 May 2026 14:12:05 |
| Eccentricity: | 0.0000090 |
| inclination: | 0.0273° |
| perigee height: | 35786 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 72.2208° |
| argument of perigee: | 271.0108° |
| revolutions per day: | 1.00272065 |
| mean anomaly at epoch: | 142.9093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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