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 26106.64680551 +.00000000 +00000-0 +15339-3 0 00004
2 10114 97.5808 280.2809 0008087 140.1080 220.0765 15.46545150 00
| Epoch (UTC): | 16 April 2026 15:31:23 |
| Eccentricity: | 0.0008087 |
| inclination: | 97.5808° |
| perigee height: | 421 km |
| apogee height: | 432 km |
| right ascension of ascending node: | 280.2809° |
| argument of perigee: | 140.1080° |
| revolutions per day: | 15.46545150 |
| mean anomaly at epoch: | 220.0765° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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