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 05681U 26133.50861791 +.00000000 +00000-0 +19662-4 0 00003
2 05681 69.9888 77.4112 0010048 227.2916 132.7333 13.74640983 01
| Epoch (UTC): | 13 May 2026 12:12:24 |
| Eccentricity: | 0.0010048 |
| inclination: | 69.9888° |
| perigee height: | 976 km |
| apogee height: | 990 km |
| right ascension of ascending node: | 77.4112° |
| argument of perigee: | 227.2916° |
| revolutions per day: | 13.74640983 |
| mean anomaly at epoch: | 132.7333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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