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 26545U 26142.08925130 +.00000000 +00000-0 +80833-4 0 00004
2 26545 64.5523 19.4999 0042325 304.9307 54.7831 14.93102409 03
| Epoch (UTC): | 22 May 2026 02:08:31 |
| Eccentricity: | 0.0042325 |
| inclination: | 64.5523° |
| perigee height: | 559 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 19.4999° |
| argument of perigee: | 304.9307° |
| revolutions per day: | 14.93102409 |
| mean anomaly at epoch: | 54.7831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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