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 57616U 26145.33994608 +.00000000 +00000-0 +14948-4 0 00008
2 57616 43.0063 8.3097 0001691 245.9370 114.1305 15.27583465 08
| Epoch (UTC): | 25 May 2026 08:09:31 |
| Eccentricity: | 0.0001691 |
| inclination: | 43.0063° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 8.3097° |
| argument of perigee: | 245.9370° |
| revolutions per day: | 15.27583465 |
| mean anomaly at epoch: | 114.1305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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