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 37387U 26145.56656350 +.00000000 +00000-0 +52070-4 0 00003
2 37387 98.7649 213.1634 0010499 327.5541 32.4990 14.21606839 00
| Epoch (UTC): | 25 May 2026 13:35:51 |
| Eccentricity: | 0.0010499 |
| inclination: | 98.7649° |
| perigee height: | 812 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 213.1634° |
| argument of perigee: | 327.5541° |
| revolutions per day: | 14.21606839 |
| mean anomaly at epoch: | 32.4990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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