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 68172U 26145.34341449 +.00000000 +00000-0 +80904-3 0 00001
2 68172 53.1591 270.3877 0001711 90.8320 269.2880 15.38847724 00
| Epoch (UTC): | 25 May 2026 08:14:31 |
| Eccentricity: | 0.0001711 |
| inclination: | 53.1591° |
| perigee height: | 448 km |
| apogee height: | 451 km |
| right ascension of ascending node: | 270.3877° |
| argument of perigee: | 90.8320° |
| revolutions per day: | 15.38847724 |
| mean anomaly at epoch: | 269.2880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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