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 57639U 26145.36685644 +.00000000 +00000-0 +64006-4 0 00003
2 57639 43.0078 19.4708 0001669 264.2265 95.8397 15.27583154 04
| Epoch (UTC): | 25 May 2026 08:48:16 |
| Eccentricity: | 0.0001669 |
| inclination: | 43.0078° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 19.4708° |
| argument of perigee: | 264.2265° |
| revolutions per day: | 15.27583154 |
| mean anomaly at epoch: | 95.8397° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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