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 11511U 26100.12008920 +.00000000 +00000-0 +62667-4 0 00004
2 11511 74.0354 154.6793 0016108 328.0009 32.0165 14.38292779 06
| Epoch (UTC): | 10 April 2026 02:52:55 |
| Eccentricity: | 0.0016108 |
| inclination: | 74.0354° |
| perigee height: | 753 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 154.6793° |
| argument of perigee: | 328.0009° |
| revolutions per day: | 14.38292779 |
| mean anomaly at epoch: | 32.0165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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