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 26017.26274162 +.00000000 +00000-0 +58985-4 0 00009
2 00876 65.0597 51.6902 0146473 316.3528 42.6061 14.65611435 06
| Epoch (UTC): | 17 January 2026 06:18:20 |
| Eccentricity: | 0.0146473 |
| inclination: | 65.0597° |
| perigee height: | 572 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 51.6902° |
| argument of perigee: | 316.3528° |
| revolutions per day: | 14.65611435 |
| mean anomaly at epoch: | 42.6061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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