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 68675U 26145.58562800 +.00000000 +00000-0 +73270-3 0 00009
2 68675 97.2868 17.1724 0002234 85.6271 274.5227 15.33451979 02
| Epoch (UTC): | 25 May 2026 14:03:18 |
| Eccentricity: | 0.0002234 |
| inclination: | 97.2868° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 17.1724° |
| argument of perigee: | 85.6271° |
| revolutions per day: | 15.33451979 |
| mean anomaly at epoch: | 274.5227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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