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 37238U 26145.52553844 +.00000000 +00000-0 +00000-0 0 00000
2 37238 0.0060 285.7198 0002520 136.4710 76.1252 1.00272802 07
| Epoch (UTC): | 25 May 2026 12:36:46 |
| Eccentricity: | 0.0002520 |
| inclination: | 0.0060° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 285.7198° |
| argument of perigee: | 136.4710° |
| revolutions per day: | 1.00272802 |
| mean anomaly at epoch: | 76.1252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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