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 26087.95785828 +.00000000 +00000-0 +22902-4 0 00007
2 05681 69.9893 171.4013 0010961 271.1164 88.8674 13.74637301 08
| Epoch (UTC): | 28 March 2026 22:59:18 |
| Eccentricity: | 0.0010961 |
| inclination: | 69.9893° |
| perigee height: | 975 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 171.4013° |
| argument of perigee: | 271.1164° |
| revolutions per day: | 13.74637301 |
| mean anomaly at epoch: | 88.8674° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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