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 68638U 26144.75406826 +.00000000 +00000-0 +41547-4 0 00004
2 68638 88.9881 323.4131 0011046 77.0057 283.2340 13.73113721 01
| Epoch (UTC): | 24 May 2026 18:05:51 |
| Eccentricity: | 0.0011046 |
| inclination: | 88.9881° |
| perigee height: | 980 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 323.4131° |
| argument of perigee: | 77.0057° |
| revolutions per day: | 13.73113721 |
| mean anomaly at epoch: | 283.2340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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