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 63251U 26145.64272346 +.00000000 +00000-0 +21874-3 0 00007
2 63251 97.6880 37.5401 0001800 334.3949 25.7182 14.95263394 02
| Epoch (UTC): | 25 May 2026 15:25:31 |
| Eccentricity: | 0.0001800 |
| inclination: | 97.6880° |
| perigee height: | 580 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 37.5401° |
| argument of perigee: | 334.3949° |
| revolutions per day: | 14.95263394 |
| mean anomaly at epoch: | 25.7182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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