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 10114U 26160.26513861 +.00000000 +00000-0 +19503-3 0 00008
2 10114 97.5844 336.4239 0005776 320.0654 40.0170 15.47718288 04
| Epoch (UTC): | 09 June 2026 06:21:47 |
| Eccentricity: | 0.0005776 |
| inclination: | 97.5844° |
| perigee height: | 419 km |
| apogee height: | 427 km |
| right ascension of ascending node: | 336.4239° |
| argument of perigee: | 320.0654° |
| revolutions per day: | 15.47718288 |
| mean anomaly at epoch: | 40.0170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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