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 26017.29687541 +.00000000 +00000-0 +66713-4 0 00000
2 00877 65.0773 121.9034 0076820 308.6407 50.7833 14.61307605 02
| Epoch (UTC): | 17 January 2026 07:07:30 |
| Eccentricity: | 0.0076820 |
| inclination: | 65.0773° |
| perigee height: | 635 km |
| apogee height: | 743 km |
| right ascension of ascending node: | 121.9034° |
| argument of perigee: | 308.6407° |
| revolutions per day: | 14.61307605 |
| mean anomaly at epoch: | 50.7833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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