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 68674U 26145.39259675 +.00000000 +00000-0 +29256-3 0 00005
2 68674 97.2878 16.9741 0001699 122.7481 237.3926 15.33390507 00
| Epoch (UTC): | 25 May 2026 09:25:20 |
| Eccentricity: | 0.0001699 |
| inclination: | 97.2878° |
| perigee height: | 465 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 16.9741° |
| argument of perigee: | 122.7481° |
| revolutions per day: | 15.33390507 |
| mean anomaly at epoch: | 237.3926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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