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 68602U 26145.58335647 +.00000000 +00000-0 -23686-1 0 00001
2 68602 97.2843 345.0658 0001538 69.1384 7.7408 15.62942541 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001538 |
| inclination: | 97.2843° |
| perigee height: | 378 km |
| apogee height: | 380 km |
| right ascension of ascending node: | 345.0658° |
| argument of perigee: | 69.1384° |
| revolutions per day: | 15.62942541 |
| mean anomaly at epoch: | 7.7408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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