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 27540U 26028.31155959 +.00000000 +00000-0 +00000-0 0 00007
2 27540 90.7723 353.9215 8648083 264.4469 335.4560 0.37582660 01
| Epoch (UTC): | 28 January 2026 07:28:38 |
| Eccentricity: | 0.8648083 |
| inclination: | 90.7723° |
| perigee height: | 4587 km |
| apogee height: | 144877 km |
| right ascension of ascending node: | 353.9215° |
| argument of perigee: | 264.4469° |
| revolutions per day: | 0.37582660 |
| mean anomaly at epoch: | 335.4560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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