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 56322U 26144.97336287 +.00000000 +00000-0 -51548-3 0 00000
2 56322 97.4480 144.9532 0001581 71.8765 288.2634 15.05687182 05
| Epoch (UTC): | 24 May 2026 23:21:38 |
| Eccentricity: | 0.0001581 |
| inclination: | 97.4480° |
| perigee height: | 548 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 144.9532° |
| argument of perigee: | 71.8765° |
| revolutions per day: | 15.05687182 |
| mean anomaly at epoch: | 288.2634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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