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 27561U 26072.89118852 +.00000000 +00000-0 +10548-3 0 00004
2 27561 98.4714 291.7970 0045288 64.8277 295.7608 14.58492942 07
| Epoch (UTC): | 13 March 2026 21:23:18 |
| Eccentricity: | 0.0045288 |
| inclination: | 98.4714° |
| perigee height: | 666 km |
| apogee height: | 730 km |
| right ascension of ascending node: | 291.7970° |
| argument of perigee: | 64.8277° |
| revolutions per day: | 14.58492942 |
| mean anomaly at epoch: | 295.7608° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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