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 37743U 26145.32193741 +.00000000 +00000-0 +25519-4 0 00001
2 37743 51.9962 265.2604 0000551 119.3014 258.9153 12.62264450 08
| Epoch (UTC): | 25 May 2026 07:43:35 |
| Eccentricity: | 0.0000551 |
| inclination: | 51.9962° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 265.2604° |
| argument of perigee: | 119.3014° |
| revolutions per day: | 12.62264450 |
| mean anomaly at epoch: | 258.9153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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