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 00877U 26128.16034918 +.00000000 +00000-0 +41113-4 0 00000
2 00877 65.0752 156.8737 0081283 273.6046 85.5761 14.61406076 03
| Epoch (UTC): | 08 May 2026 03:50:54 |
| Eccentricity: | 0.0081283 |
| inclination: | 65.0752° |
| perigee height: | 631 km |
| apogee height: | 746 km |
| right ascension of ascending node: | 156.8737° |
| argument of perigee: | 273.6046° |
| revolutions per day: | 14.61406076 |
| mean anomaly at epoch: | 85.5761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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