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 26065U 26154.45299310 +.00000000 +00000-0 +91118-4 0 00007
2 26065 100.1946 92.4662 0036716 72.5025 288.0164 14.38230774 03
| Epoch (UTC): | 03 June 2026 10:52:18 |
| Eccentricity: | 0.0036716 |
| inclination: | 100.1946° |
| perigee height: | 738 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 92.4662° |
| argument of perigee: | 72.5025° |
| revolutions per day: | 14.38230774 |
| mean anomaly at epoch: | 288.0164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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