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 35932U 26032.27784351 +.00000000 +00000-0 +27462-3 0 00009
2 35932 98.4136 297.7694 0005570 279.6400 80.4171 14.62148311 06
| Epoch (UTC): | 01 February 2026 06:40:05 |
| Eccentricity: | 0.0005570 |
| inclination: | 98.4136° |
| perigee height: | 682 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 297.7694° |
| argument of perigee: | 279.6400° |
| revolutions per day: | 14.62148311 |
| mean anomaly at epoch: | 80.4171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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