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 37826U 26145.49719830 +.00000000 +00000-0 +00000-0 0 00008
2 37826 0.0583 80.4796 0002730 339.3675 285.2262 1.00272309 07
| Epoch (UTC): | 25 May 2026 11:55:57 |
| Eccentricity: | 0.0002730 |
| inclination: | 0.0583° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 80.4796° |
| argument of perigee: | 339.3675° |
| revolutions per day: | 1.00272309 |
| mean anomaly at epoch: | 285.2262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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