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 37776U 26145.53420514 +.00000000 +00000-0 +00000-0 0 00005
2 37776 0.0201 5.4341 0000155 110.6511 69.3071 1.00272477 04
| Epoch (UTC): | 25 May 2026 12:49:15 |
| Eccentricity: | 0.0000155 |
| inclination: | 0.0201° |
| perigee height: | 35786 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 5.4341° |
| argument of perigee: | 110.6511° |
| revolutions per day: | 1.00272477 |
| mean anomaly at epoch: | 69.3071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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