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 37810U 26145.58771513 +.00000000 +00000-0 +00000-0 0 00007
2 37810 0.0494 351.4665 0003256 93.9676 29.3410 1.00272832 08
| Epoch (UTC): | 25 May 2026 14:06:18 |
| Eccentricity: | 0.0003256 |
| inclination: | 0.0494° |
| perigee height: | 35773 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 351.4665° |
| argument of perigee: | 93.9676° |
| revolutions per day: | 1.00272832 |
| mean anomaly at epoch: | 29.3410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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