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 37740U 26145.32928823 +.00000000 +00000-0 +11912-3 0 00006
2 37740 52.0234 348.5055 0000886 90.4532 80.3028 12.62268177 07
| Epoch (UTC): | 25 May 2026 07:54:10 |
| Eccentricity: | 0.0000886 |
| inclination: | 52.0234° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 348.5055° |
| argument of perigee: | 90.4532° |
| revolutions per day: | 12.62268177 |
| mean anomaly at epoch: | 80.3028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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