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 57187U 26145.63938883 +.00000000 +00000-0 +33347-3 0 00000
2 57187 97.5103 209.3375 0010162 163.2575 196.9000 15.26163051 08
| Epoch (UTC): | 25 May 2026 15:20:43 |
| Eccentricity: | 0.0010162 |
| inclination: | 97.5103° |
| perigee height: | 480 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 209.3375° |
| argument of perigee: | 163.2575° |
| revolutions per day: | 15.26163051 |
| mean anomaly at epoch: | 196.9000° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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