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 68271U 26145.21375802 +.00000000 +00000-0 +76539-3 0 00006
2 68271 53.1598 322.6461 0001391 96.5228 263.5933 15.34403060 04
| Epoch (UTC): | 25 May 2026 05:07:48 |
| Eccentricity: | 0.0001391 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 322.6461° |
| argument of perigee: | 96.5228° |
| revolutions per day: | 15.34403060 |
| mean anomaly at epoch: | 263.5933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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