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 00877U 26019.69216780 +.00000000 +00000-0 +80000-4 0 00004
2 00877 65.0771 114.8816 0076989 307.8676 51.5476 14.61309475 03
| Epoch (UTC): | 19 January 2026 16:36:43 |
| Eccentricity: | 0.0076989 |
| inclination: | 65.0771° |
| perigee height: | 635 km |
| apogee height: | 743 km |
| right ascension of ascending node: | 114.8816° |
| argument of perigee: | 307.8676° |
| revolutions per day: | 14.61309475 |
| mean anomaly at epoch: | 51.5476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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