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 26073.91417412 +.00000000 +00000-0 +10403-3 0 00000
2 27640 98.7160 82.2282 0014963 122.2955 237.9673 14.19915036 01
| Epoch (UTC): | 14 March 2026 21:56:24 |
| Eccentricity: | 0.0014963 |
| inclination: | 98.7160° |
| perigee height: | 815 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 82.2282° |
| argument of perigee: | 122.2955° |
| revolutions per day: | 14.19915036 |
| mean anomaly at epoch: | 237.9673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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