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 00876U 26072.87350221 +.00000000 +00000-0 +58006-4 0 00002
2 00876 65.0580 247.3704 0150254 296.5359 62.0404 14.65677992 02
| Epoch (UTC): | 13 March 2026 20:57:50 |
| Eccentricity: | 0.0150254 |
| inclination: | 65.0580° |
| perigee height: | 569 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 247.3704° |
| argument of perigee: | 296.5359° |
| revolutions per day: | 14.65677992 |
| mean anomaly at epoch: | 62.0404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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