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 27599U 26087.87069951 +.00000000 +00000-0 +98514-4 0 00004
2 27599 98.8086 54.5380 0009466 181.4839 178.6316 14.30813813 01
| Epoch (UTC): | 28 March 2026 20:53:48 |
| Eccentricity: | 0.0009466 |
| inclination: | 98.8086° |
| perigee height: | 782 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 54.5380° |
| argument of perigee: | 181.4839° |
| revolutions per day: | 14.30813813 |
| mean anomaly at epoch: | 178.6316° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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