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 68420U 26145.63316929 +.00000000 +00000-0 +47819-3 0 00002
2 68420 97.4462 104.4585 0002019 51.1474 308.9941 15.19284360 08
| Epoch (UTC): | 25 May 2026 15:11:45 |
| Eccentricity: | 0.0002019 |
| inclination: | 97.4462° |
| perigee height: | 507 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 104.4585° |
| argument of perigee: | 51.1474° |
| revolutions per day: | 15.19284360 |
| mean anomaly at epoch: | 308.9941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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