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 35933U 26071.51691406 +.00000000 +00000-0 +26159-3 0 00000
2 35933 98.4025 337.5444 0005513 154.7579 205.3891 14.61540877 06
| Epoch (UTC): | 12 March 2026 12:24:21 |
| Eccentricity: | 0.0005513 |
| inclination: | 98.4025° |
| perigee height: | 684 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 337.5444° |
| argument of perigee: | 154.7579° |
| revolutions per day: | 14.61540877 |
| mean anomaly at epoch: | 205.3891° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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