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 27438U 26145.48587426 +.00000000 +00000-0 +00000-0 0 00009
2 27438 6.6992 70.0710 0004069 3.6256 207.0839 1.00273871 02
| Epoch (UTC): | 25 May 2026 11:39:39 |
| Eccentricity: | 0.0004069 |
| inclination: | 6.6992° |
| perigee height: | 35769 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 70.0710° |
| argument of perigee: | 3.6256° |
| revolutions per day: | 1.00273871 |
| mean anomaly at epoch: | 207.0839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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