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 27560U 26039.23359719 +.00000000 +00000-0 +12403-3 0 00005
2 27560 98.4552 253.2090 0039327 58.1791 77.7471 14.61646702 01
| Epoch (UTC): | 08 February 2026 05:36:22 |
| Eccentricity: | 0.0039327 |
| inclination: | 98.4552° |
| perigee height: | 660 km |
| apogee height: | 716 km |
| right ascension of ascending node: | 253.2090° |
| argument of perigee: | 58.1791° |
| revolutions per day: | 14.61646702 |
| mean anomaly at epoch: | 77.7471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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