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 68458U 26144.84233523 +.00000000 +00000-0 +34426-3 0 00003
2 68458 97.4464 103.5242 0007053 139.2688 220.9074 15.17368527 05
| Epoch (UTC): | 24 May 2026 20:12:57 |
| Eccentricity: | 0.0007053 |
| inclination: | 97.4464° |
| perigee height: | 509 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 103.5242° |
| argument of perigee: | 139.2688° |
| revolutions per day: | 15.17368527 |
| mean anomaly at epoch: | 220.9074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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