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 68447U 26145.32577036 +.00000000 +00000-0 +36200-3 0 00007
2 68447 97.4504 104.1320 0003473 89.7733 270.3899 15.18575832 08
| Epoch (UTC): | 25 May 2026 07:49:06 |
| Eccentricity: | 0.0003473 |
| inclination: | 97.4504° |
| perigee height: | 508 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 104.1320° |
| argument of perigee: | 89.7733° |
| revolutions per day: | 15.18575832 |
| mean anomaly at epoch: | 270.3899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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