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 26017.63906028 +.00000000 +00000-0 +63852-4 0 00003
2 00877 65.0772 120.9002 0076847 308.5278 50.8949 14.61307683 04
| Epoch (UTC): | 17 January 2026 15:20:14 |
| Eccentricity: | 0.0076847 |
| inclination: | 65.0772° |
| perigee height: | 635 km |
| apogee height: | 743 km |
| right ascension of ascending node: | 120.9002° |
| argument of perigee: | 308.5278° |
| revolutions per day: | 14.61307683 |
| mean anomaly at epoch: | 50.8949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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