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 26072.92764286 +.00000000 +00000-0 +10141-3 0 00003
2 27640 98.7160 81.2566 0014944 124.9983 235.2598 14.19914591 06
| Epoch (UTC): | 13 March 2026 22:15:48 |
| Eccentricity: | 0.0014944 |
| inclination: | 98.7160° |
| perigee height: | 815 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 81.2566° |
| argument of perigee: | 124.9983° |
| revolutions per day: | 14.19914591 |
| mean anomaly at epoch: | 235.2598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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