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 68173U 26145.34213591 +.00000000 +00000-0 +66540-3 0 00008
2 68173 53.1590 270.3767 0001403 76.1814 283.9345 15.34411769 02
| Epoch (UTC): | 25 May 2026 08:12:40 |
| Eccentricity: | 0.0001403 |
| inclination: | 53.1590° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 270.3767° |
| argument of perigee: | 76.1814° |
| revolutions per day: | 15.34411769 |
| mean anomaly at epoch: | 283.9345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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