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 68467U 26145.61860828 +.00000000 +00000-0 +78128-3 0 00000
2 68467 97.4396 104.2788 0007958 137.6444 222.5406 15.18203506 01
| Epoch (UTC): | 25 May 2026 14:50:47 |
| Eccentricity: | 0.0007958 |
| inclination: | 97.4396° |
| perigee height: | 506 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 104.2788° |
| argument of perigee: | 137.6444° |
| revolutions per day: | 15.18203506 |
| mean anomaly at epoch: | 222.5406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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