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 25758U 26065.86420522 +.00000000 +00000-0 +18958-3 0 00002
2 25758 97.9597 43.5564 0004150 102.9200 257.2462 14.55181675 07
| Epoch (UTC): | 06 March 2026 20:44:27 |
| Eccentricity: | 0.0004150 |
| inclination: | 97.9597° |
| perigee height: | 706 km |
| apogee height: | 712 km |
| right ascension of ascending node: | 43.5564° |
| argument of perigee: | 102.9200° |
| revolutions per day: | 14.55181675 |
| mean anomaly at epoch: | 257.2462° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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