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 68758U 26145.75409794 +.00000000 +00000-0 +11297-3 0 00003
2 68758 97.8015 283.4267 0011879 126.3036 233.9289 15.06400211 01
| Epoch (UTC): | 25 May 2026 18:05:54 |
| Eccentricity: | 0.0011879 |
| inclination: | 97.8015° |
| perigee height: | 539 km |
| apogee height: | 555 km |
| right ascension of ascending node: | 283.4267° |
| argument of perigee: | 126.3036° |
| revolutions per day: | 15.06400211 |
| mean anomaly at epoch: | 233.9289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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