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 57107U 26145.57145036 +.00000000 +00000-0 +34445-4 0 00006
2 57107 43.0031 207.0944 0001807 274.4532 85.6113 15.27577164 01
| Epoch (UTC): | 25 May 2026 13:42:53 |
| Eccentricity: | 0.0001807 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 207.0944° |
| argument of perigee: | 274.4532° |
| revolutions per day: | 15.27577164 |
| mean anomaly at epoch: | 85.6113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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