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 07735U 26067.79611422 +.00000000 +00000-0 +12554-3 0 00008
2 07735 114.9734 14.8365 0054286 285.2237 74.2847 14.25568594 05
| Epoch (UTC): | 08 March 2026 19:06:24 |
| Eccentricity: | 0.0054286 |
| inclination: | 114.9734° |
| perigee height: | 768 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 14.8365° |
| argument of perigee: | 285.2237° |
| revolutions per day: | 14.25568594 |
| mean anomaly at epoch: | 74.2847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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