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 68390U 26145.58335647 +.00000000 +00000-0 +11645-3 0 00008
2 68390 97.2849 289.6241 0005531 259.2442 188.4239 15.84220873 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0005531 |
| inclination: | 97.2849° |
| perigee height: | 315 km |
| apogee height: | 322 km |
| right ascension of ascending node: | 289.6241° |
| argument of perigee: | 259.2442° |
| revolutions per day: | 15.84220873 |
| mean anomaly at epoch: | 188.4239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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