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 02389U 26141.20616340 +.00000000 +00000-0 +27911-3 0 00004
2 02389 81.3275 354.8096 1014014 227.6496 123.4372 13.44641751 00
| Epoch (UTC): | 21 May 2026 04:56:52 |
| Eccentricity: | 0.1014014 |
| inclination: | 81.3275° |
| perigee height: | 335 km |
| apogee height: | 1850 km |
| right ascension of ascending node: | 354.8096° |
| argument of perigee: | 227.6496° |
| revolutions per day: | 13.44641751 |
| mean anomaly at epoch: | 123.4372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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