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 63225U 26145.42471516 +.00000000 +00000-0 +17810-3 0 00009
2 63225 97.4040 38.6762 0004371 195.2183 164.8922 15.22198224 08
| Epoch (UTC): | 25 May 2026 10:11:35 |
| Eccentricity: | 0.0004371 |
| inclination: | 97.4040° |
| perigee height: | 496 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 38.6762° |
| argument of perigee: | 195.2183° |
| revolutions per day: | 15.22198224 |
| mean anomaly at epoch: | 164.8922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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