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 57337U 26145.57898933 +.00000000 +00000-0 -54167-5 0 00007
2 57337 43.0025 178.3358 0001366 269.9320 90.1375 15.27574394 05
| Epoch (UTC): | 25 May 2026 13:53:44 |
| Eccentricity: | 0.0001366 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 178.3358° |
| argument of perigee: | 269.9320° |
| revolutions per day: | 15.27574394 |
| mean anomaly at epoch: | 90.1375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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