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 37398U 26023.21624184 +.00000000 +00000-0 +17993-2 0 00005
2 37398 62.1482 97.7407 7485784 263.7551 15.1037 2.00876999 08
| Epoch (UTC): | 23 January 2026 05:11:23 |
| Eccentricity: | 0.7485784 |
| inclination: | 62.1482° |
| perigee height: | 293 km |
| apogee height: | 40016 km |
| right ascension of ascending node: | 97.7407° |
| argument of perigee: | 263.7551° |
| revolutions per day: | 2.00876999 |
| mean anomaly at epoch: | 15.1037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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