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 33319U 26088.20279881 +.00000000 +00000-0 +57542-4 0 00000
2 33319 97.9423 307.7194 0492501 229.0186 249.5878 13.75788898 02
| Epoch (UTC): | 29 March 2026 04:52:01 |
| Eccentricity: | 0.0492501 |
| inclination: | 97.9423° |
| perigee height: | 617 km |
| apogee height: | 1341 km |
| right ascension of ascending node: | 307.7194° |
| argument of perigee: | 229.0186° |
| revolutions per day: | 13.75788898 |
| mean anomaly at epoch: | 249.5878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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