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 26067.92451436 +.00000000 +00000-0 +10610-3 0 00008
2 27640 98.7162 76.3292 0014742 138.5745 221.6552 14.19912421 01
| Epoch (UTC): | 08 March 2026 22:11:18 |
| Eccentricity: | 0.0014742 |
| inclination: | 98.7162° |
| perigee height: | 815 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 76.3292° |
| argument of perigee: | 138.5745° |
| revolutions per day: | 14.19912421 |
| mean anomaly at epoch: | 221.6552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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