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 11288U 26088.09854308 +.00000000 +00000-0 +71515-4 0 00007
2 11288 81.2180 216.5463 0024405 160.8779 199.3315 14.12319912 06
| Epoch (UTC): | 29 March 2026 02:21:54 |
| Eccentricity: | 0.0024405 |
| inclination: | 81.2180° |
| perigee height: | 834 km |
| apogee height: | 869 km |
| right ascension of ascending node: | 216.5463° |
| argument of perigee: | 160.8779° |
| revolutions per day: | 14.12319912 |
| mean anomaly at epoch: | 199.3315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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