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 57177U 26145.57691001 +.00000000 +00000-0 +30585-3 0 00001
2 57177 97.5106 204.6180 0013286 188.4796 171.6217 15.20555312 05
| Epoch (UTC): | 25 May 2026 13:50:45 |
| Eccentricity: | 0.0013286 |
| inclination: | 97.5106° |
| perigee height: | 495 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 204.6180° |
| argument of perigee: | 188.4796° |
| revolutions per day: | 15.20555312 |
| mean anomaly at epoch: | 171.6217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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