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 57467U 26145.37882638 +.00000000 +00000-0 +15982-3 0 00003
2 57467 43.0046 263.1819 0001984 266.7429 93.3196 15.27576840 02
| Epoch (UTC): | 25 May 2026 09:05:30 |
| Eccentricity: | 0.0001984 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 263.1819° |
| argument of perigee: | 266.7429° |
| revolutions per day: | 15.27576840 |
| mean anomaly at epoch: | 93.3196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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