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 56346U 26144.95675955 +.00000000 +00000-0 -38790-3 0 00006
2 56346 97.4513 144.9770 0002001 89.6621 270.4836 15.05666412 08
| Epoch (UTC): | 24 May 2026 22:57:44 |
| Eccentricity: | 0.0002001 |
| inclination: | 97.4513° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 144.9770° |
| argument of perigee: | 89.6621° |
| revolutions per day: | 15.05666412 |
| mean anomaly at epoch: | 270.4836° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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