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 26072.31396019 +.00000000 +00000-0 +11847-1 0 00009
2 59588 97.2045 12.6111 0062791 67.8385 292.9427 13.89761996 02
| Epoch (UTC): | 13 March 2026 07:32:06 |
| Eccentricity: | 0.0062791 |
| inclination: | 97.2045° |
| perigee height: | 884 km |
| apogee height: | 975 km |
| right ascension of ascending node: | 12.6111° |
| argument of perigee: | 67.8385° |
| revolutions per day: | 13.89761996 |
| mean anomaly at epoch: | 292.9427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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