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 57179U 26145.58418076 +.00000000 +00000-0 +20086-3 0 00008
2 57179 97.5109 201.7979 0014481 197.5074 162.5662 15.16281412 07
| Epoch (UTC): | 25 May 2026 14:01:13 |
| Eccentricity: | 0.0014481 |
| inclination: | 97.5109° |
| perigee height: | 507 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 201.7979° |
| argument of perigee: | 197.5074° |
| revolutions per day: | 15.16281412 |
| mean anomaly at epoch: | 162.5662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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