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 68422U 26144.85711523 +.00000000 +00000-0 +15396-3 0 00001
2 68422 97.4467 103.6572 0001715 60.6650 299.4755 15.18617793 01
| Epoch (UTC): | 24 May 2026 20:34:14 |
| Eccentricity: | 0.0001715 |
| inclination: | 97.4467° |
| perigee height: | 509 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 103.6572° |
| argument of perigee: | 60.6650° |
| revolutions per day: | 15.18617793 |
| mean anomaly at epoch: | 299.4755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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