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 57357U 26145.53545285 +.00000000 +00000-0 +94026-4 0 00000
2 57357 43.0031 167.5417 0001271 265.6182 94.4524 15.27574527 05
| Epoch (UTC): | 25 May 2026 12:51:03 |
| Eccentricity: | 0.0001271 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 167.5417° |
| argument of perigee: | 265.6182° |
| revolutions per day: | 15.27574527 |
| mean anomaly at epoch: | 94.4524° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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