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 11327U 26042.16129028 +.00000000 +00000-0 +94392-4 0 00001
2 11327 82.9494 108.7517 0026704 332.8187 45.9185 13.77196686 08
| Epoch (UTC): | 11 February 2026 03:52:15 |
| Eccentricity: | 0.0026704 |
| inclination: | 82.9494° |
| perigee height: | 954 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 108.7517° |
| argument of perigee: | 332.8187° |
| revolutions per day: | 13.77196686 |
| mean anomaly at epoch: | 45.9185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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