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 63236U 26145.41939992 +.00000000 +00000-0 +18393-3 0 00004
2 63236 97.3869 37.4969 0002543 207.5132 152.5970 15.21843392 03
| Epoch (UTC): | 25 May 2026 10:03:56 |
| Eccentricity: | 0.0002543 |
| inclination: | 97.3869° |
| perigee height: | 499 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 37.4969° |
| argument of perigee: | 207.5132° |
| revolutions per day: | 15.21843392 |
| mean anomaly at epoch: | 152.5970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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