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 27844U 26072.49788692 +.00000000 +00000-0 +20331-3 0 00000
2 27844 98.6777 82.2494 0010739 102.5935 257.6446 14.24269872 04
| Epoch (UTC): | 13 March 2026 11:56:57 |
| Eccentricity: | 0.0010739 |
| inclination: | 98.6777° |
| perigee height: | 803 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 82.2494° |
| argument of perigee: | 102.5935° |
| revolutions per day: | 14.24269872 |
| mean anomaly at epoch: | 257.6446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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