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 68481U 26145.63403333 +.00000000 +00000-0 +13621-3 0 00009
2 68481 97.7660 104.3076 0003923 50.2672 309.8892 14.92086772 09
| Epoch (UTC): | 25 May 2026 15:13:00 |
| Eccentricity: | 0.0003923 |
| inclination: | 97.7660° |
| perigee height: | 589 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 104.3076° |
| argument of perigee: | 50.2672° |
| revolutions per day: | 14.92086772 |
| mean anomaly at epoch: | 309.8892° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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