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 27640U 26141.98412926 +.00000000 +00000-0 +52561-4 0 00000
2 27640 98.7131 149.2689 0012846 290.3043 69.6753 14.19936830 01
| Epoch (UTC): | 21 May 2026 23:37:08 |
| Eccentricity: | 0.0012846 |
| inclination: | 98.7131° |
| perigee height: | 816 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 149.2689° |
| argument of perigee: | 290.3043° |
| revolutions per day: | 14.19936830 |
| mean anomaly at epoch: | 69.6753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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