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 26040.94026784 +.00000000 +00000-0 +95747-4 0 00002
2 00876 65.0609 341.7298 0148301 307.8990 50.8777 14.65651052 05
| Epoch (UTC): | 09 February 2026 22:33:59 |
| Eccentricity: | 0.0148301 |
| inclination: | 65.0609° |
| perigee height: | 570 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 341.7298° |
| argument of perigee: | 307.8990° |
| revolutions per day: | 14.65651052 |
| mean anomaly at epoch: | 50.8777° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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