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 63223U 26145.27827155 +.00000000 +00000-0 +22973-3 0 00000
2 63223 97.3962 38.4750 0003133 188.2011 171.9175 15.22960049 01
| Epoch (UTC): | 25 May 2026 06:40:42 |
| Eccentricity: | 0.0003133 |
| inclination: | 97.3962° |
| perigee height: | 495 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 38.4750° |
| argument of perigee: | 188.2011° |
| revolutions per day: | 15.22960049 |
| mean anomaly at epoch: | 171.9175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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