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 11321U 26088.18749502 +.00000000 +00000-0 +40297-4 0 00007
2 11321 82.9249 153.9062 0017410 260.1493 152.8073 13.76804786 04
| Epoch (UTC): | 29 March 2026 04:29:59 |
| Eccentricity: | 0.0017410 |
| inclination: | 82.9249° |
| perigee height: | 962 km |
| apogee height: | 988 km |
| right ascension of ascending node: | 153.9062° |
| argument of perigee: | 260.1493° |
| revolutions per day: | 13.76804786 |
| mean anomaly at epoch: | 152.8073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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