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 10677U 26088.19644498 +.00000000 +00000-0 +75349-4 0 00005
2 10677 74.0367 131.8706 0013857 140.9841 219.2318 14.41722620 02
| Epoch (UTC): | 29 March 2026 04:42:52 |
| Eccentricity: | 0.0013857 |
| inclination: | 74.0367° |
| perigee height: | 743 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 131.8706° |
| argument of perigee: | 140.9841° |
| revolutions per day: | 14.41722620 |
| mean anomaly at epoch: | 219.2318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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