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 33499U 26069.88193252 +.00000000 +00000-0 +25323-3 0 00000
2 33499 98.1179 350.7954 0006508 245.8404 114.2128 14.82835603 03
| Epoch (UTC): | 10 March 2026 21:09:58 |
| Eccentricity: | 0.0006508 |
| inclination: | 98.1179° |
| perigee height: | 616 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 350.7954° |
| argument of perigee: | 245.8404° |
| revolutions per day: | 14.82835603 |
| mean anomaly at epoch: | 114.2128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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