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 56478U 26145.42545338 +.00000000 +00000-0 +46079-5 0 00006
2 56478 69.9988 290.9715 0002759 266.3110 93.7734 14.98331116 06
| Epoch (UTC): | 25 May 2026 10:12:39 |
| Eccentricity: | 0.0002759 |
| inclination: | 69.9988° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 290.9715° |
| argument of perigee: | 266.3110° |
| revolutions per day: | 14.98331116 |
| mean anomaly at epoch: | 93.7734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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