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 57054U 26144.98377527 +.00000000 +00000-0 +66754-5 0 00002
2 57054 43.0042 39.5292 0001298 251.4637 108.6074 15.27584291 04
| Epoch (UTC): | 24 May 2026 23:36:38 |
| Eccentricity: | 0.0001298 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 39.5292° |
| argument of perigee: | 251.4637° |
| revolutions per day: | 15.27584291 |
| mean anomaly at epoch: | 108.6074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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