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 26092U 26150.53696146 +.00000000 +00000-0 +24870-3 0 00000
2 26092 100.2079 173.4250 0031279 192.6853 167.3550 14.48803312 09
| Epoch (UTC): | 30 May 2026 12:53:13 |
| Eccentricity: | 0.0031279 |
| inclination: | 100.2079° |
| perigee height: | 707 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 173.4250° |
| argument of perigee: | 192.6853° |
| revolutions per day: | 14.48803312 |
| mean anomaly at epoch: | 167.3550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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