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 37481U 26140.46076036 +.00000000 +00000-0 +00000-0 0 00001
2 37481 4.4763 53.1307 0002265 358.6780 43.9878 1.00271788 03
| Epoch (UTC): | 20 May 2026 11:03:29 |
| Eccentricity: | 0.0002265 |
| inclination: | 4.4763° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 53.1307° |
| argument of perigee: | 358.6780° |
| revolutions per day: | 1.00271788 |
| mean anomaly at epoch: | 43.9878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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