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 26017.80862884 +.00000000 +00000-0 +58351-4 0 00000
2 00876 65.0597 50.0773 0146500 316.1566 42.7980 14.65611772 01
| Epoch (UTC): | 17 January 2026 19:24:25 |
| Eccentricity: | 0.0146500 |
| inclination: | 65.0597° |
| perigee height: | 572 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 50.0773° |
| argument of perigee: | 316.1566° |
| revolutions per day: | 14.65611772 |
| mean anomaly at epoch: | 42.7980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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