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 57340U 26145.40081553 +.00000000 +00000-0 +14378-4 0 00003
2 57340 43.0007 179.5802 0000933 281.0480 79.0266 15.27575583 03
| Epoch (UTC): | 25 May 2026 09:37:10 |
| Eccentricity: | 0.0000933 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 179.5802° |
| argument of perigee: | 281.0480° |
| revolutions per day: | 15.27575583 |
| mean anomaly at epoch: | 79.0266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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