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 68037U 26145.34021742 +.00000000 +00000-0 +91748-3 0 00000
2 68037 97.2837 94.4102 0002011 110.2056 249.9403 15.33455583 04
| Epoch (UTC): | 25 May 2026 08:09:54 |
| Eccentricity: | 0.0002011 |
| inclination: | 97.2837° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.4102° |
| argument of perigee: | 110.2056° |
| revolutions per day: | 15.33455583 |
| mean anomaly at epoch: | 249.9403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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