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 26087.85963243 +.00000000 +00000-0 +82993-4 0 00003
2 07735 114.9757 70.4558 0054658 280.1651 79.3269 14.25577079 01
| Epoch (UTC): | 28 March 2026 20:37:52 |
| Eccentricity: | 0.0054658 |
| inclination: | 114.9757° |
| perigee height: | 767 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 70.4558° |
| argument of perigee: | 280.1651° |
| revolutions per day: | 14.25577079 |
| mean anomaly at epoch: | 79.3269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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