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 68416U 26145.36986470 +.00000000 +00000-0 +33171-3 0 00007
2 68416 97.4528 104.2412 0002788 40.3170 319.8270 15.19141544 01
| Epoch (UTC): | 25 May 2026 08:52:36 |
| Eccentricity: | 0.0002788 |
| inclination: | 97.4528° |
| perigee height: | 507 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 104.2412° |
| argument of perigee: | 40.3170° |
| revolutions per day: | 15.19141544 |
| mean anomaly at epoch: | 319.8270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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