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 68225U 26145.37460058 +.00000000 +00000-0 +80162-3 0 00007
2 68225 97.2866 20.8737 0001962 89.6303 270.5165 15.33451268 01
| Epoch (UTC): | 25 May 2026 08:59:25 |
| Eccentricity: | 0.0001962 |
| inclination: | 97.2866° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 20.8737° |
| argument of perigee: | 89.6303° |
| revolutions per day: | 15.33451268 |
| mean anomaly at epoch: | 270.5165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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