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 68038U 26145.34838134 +.00000000 +00000-0 +83679-3 0 00006
2 68038 97.2851 94.4004 0001804 97.5777 262.5671 15.33443154 07
| Epoch (UTC): | 25 May 2026 08:21:40 |
| Eccentricity: | 0.0001804 |
| inclination: | 97.2851° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.4004° |
| argument of perigee: | 97.5777° |
| revolutions per day: | 15.33443154 |
| mean anomaly at epoch: | 262.5671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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