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 68039U 26145.61211275 +.00000000 +00000-0 +57555-3 0 00002
2 68039 97.2843 94.6486 0001509 85.6522 274.4893 15.33459233 06
| Epoch (UTC): | 25 May 2026 14:41:26 |
| Eccentricity: | 0.0001509 |
| inclination: | 97.2843° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.6486° |
| argument of perigee: | 85.6522° |
| revolutions per day: | 15.33459233 |
| mean anomaly at epoch: | 274.4893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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