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 57920U 26145.55966441 +.00000000 +00000-0 +16102-3 0 00007
2 57920 43.0061 251.1469 0001750 262.2576 97.8077 15.27580493 02
| Epoch (UTC): | 25 May 2026 13:25:55 |
| Eccentricity: | 0.0001750 |
| inclination: | 43.0061° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 251.1469° |
| argument of perigee: | 262.2576° |
| revolutions per day: | 15.27580493 |
| mean anomaly at epoch: | 97.8077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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