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 57400U 26145.56370675 +.00000000 +00000-0 +21641-3 0 00003
2 57400 97.2599 196.5288 0003876 174.7251 185.4031 15.29506727 05
| Epoch (UTC): | 25 May 2026 13:31:44 |
| Eccentricity: | 0.0003876 |
| inclination: | 97.2599° |
| perigee height: | 475 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 196.5288° |
| argument of perigee: | 174.7251° |
| revolutions per day: | 15.29506727 |
| mean anomaly at epoch: | 185.4031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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