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 28932U 26162.38575122 +.00000000 +00000-0 +27216-3 0 00008
2 28932 98.2553 317.6909 0049634 282.5768 76.9915 15.17987423 01
| Epoch (UTC): | 11 June 2026 09:15:28 |
| Eccentricity: | 0.0049634 |
| inclination: | 98.2553° |
| perigee height: | 478 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 317.6909° |
| argument of perigee: | 282.5768° |
| revolutions per day: | 15.17987423 |
| mean anomaly at epoch: | 76.9915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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