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 57189U 26145.60168212 +.00000000 +00000-0 +47872-3 0 00008
2 57189 97.5102 214.6466 0008611 144.7595 215.4219 15.35189717 07
| Epoch (UTC): | 25 May 2026 14:26:25 |
| Eccentricity: | 0.0008611 |
| inclination: | 97.5102° |
| perigee height: | 454 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 214.6466° |
| argument of perigee: | 144.7595° |
| revolutions per day: | 15.35189717 |
| mean anomaly at epoch: | 215.4219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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