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 68057U 26145.18189005 +.00000000 +00000-0 +97418-3 0 00001
2 68057 53.1581 52.8712 0001141 79.1716 280.9415 15.34430109 03
| Epoch (UTC): | 25 May 2026 04:21:55 |
| Eccentricity: | 0.0001141 |
| inclination: | 53.1581° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 52.8712° |
| argument of perigee: | 79.1716° |
| revolutions per day: | 15.34430109 |
| mean anomaly at epoch: | 280.9415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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