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 37836U 26145.58693512 +.00000000 +00000-0 +00000-0 0 00007
2 37836 0.0460 0.7255 0005913 69.3010 40.4416 1.00270834 09
| Epoch (UTC): | 25 May 2026 14:05:11 |
| Eccentricity: | 0.0005913 |
| inclination: | 0.0460° |
| perigee height: | 35762 km |
| apogee height: | 35812 km |
| right ascension of ascending node: | 0.7255° |
| argument of perigee: | 69.3010° |
| revolutions per day: | 1.00270834 |
| mean anomaly at epoch: | 40.4416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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