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 68168U 26145.64229257 +.00000000 +00000-0 +62274-4 0 00002
2 68168 53.1590 268.7158 0000844 37.0457 323.0608 15.42161382 08
| Epoch (UTC): | 25 May 2026 15:24:54 |
| Eccentricity: | 0.0000844 |
| inclination: | 53.1590° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 268.7158° |
| argument of perigee: | 37.0457° |
| revolutions per day: | 15.42161382 |
| mean anomaly at epoch: | 323.0608° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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