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 59588U 26127.76993993 +.00000000 +00000-0 -61731-2 0 00002
2 59588 97.1764 55.6118 0042003 340.4086 19.5464 13.92386108 01
| Epoch (UTC): | 07 May 2026 18:28:42 |
| Eccentricity: | 0.0042003 |
| inclination: | 97.1764° |
| perigee height: | 890 km |
| apogee height: | 951 km |
| right ascension of ascending node: | 55.6118° |
| argument of perigee: | 340.4086° |
| revolutions per day: | 13.92386108 |
| mean anomaly at epoch: | 19.5464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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