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 26068.49763803 +.00000000 +00000-0 +11696-3 0 00003
2 07735 114.9733 16.7811 0054289 285.0522 74.4556 14.25568889 05
| Epoch (UTC): | 09 March 2026 11:56:35 |
| Eccentricity: | 0.0054289 |
| inclination: | 114.9733° |
| perigee height: | 768 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 16.7811° |
| argument of perigee: | 285.0522° |
| revolutions per day: | 14.25568889 |
| mean anomaly at epoch: | 74.4556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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