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 56490U 26145.36264381 +.00000000 +00000-0 -46930-4 0 00005
2 56490 69.9991 271.2804 0002903 266.3764 93.7063 14.98338143 03
| Epoch (UTC): | 25 May 2026 08:42:12 |
| Eccentricity: | 0.0002903 |
| inclination: | 69.9991° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 271.2804° |
| argument of perigee: | 266.3764° |
| revolutions per day: | 14.98338143 |
| mean anomaly at epoch: | 93.7063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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