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 56890U 26145.33906799 +.00000000 +00000-0 +24225-3 0 00003
2 56890 43.0033 15.6665 0000994 285.9545 74.1197 15.27562365 03
| Epoch (UTC): | 25 May 2026 08:08:15 |
| Eccentricity: | 0.0000994 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 15.6665° |
| argument of perigee: | 285.9545° |
| revolutions per day: | 15.27562365 |
| mean anomaly at epoch: | 74.1197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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