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 68738U 26145.37735138 +.00000000 +00000-0 +60607-3 0 00002
2 68738 97.2857 8.9128 0000411 126.1129 234.0160 15.49221443 09
| Epoch (UTC): | 25 May 2026 09:03:23 |
| Eccentricity: | 0.0000411 |
| inclination: | 97.2857° |
| perigee height: | 419 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 8.9128° |
| argument of perigee: | 126.1129° |
| revolutions per day: | 15.49221443 |
| mean anomaly at epoch: | 234.0160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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