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 63254U 26145.46603126 +.00000000 +00000-0 +29529-3 0 00009
2 63254 97.6964 46.7885 0000909 315.8835 44.2322 15.11650048 00
| Epoch (UTC): | 25 May 2026 11:11:05 |
| Eccentricity: | 0.0000909 |
| inclination: | 97.6964° |
| perigee height: | 531 km |
| apogee height: | 532 km |
| right ascension of ascending node: | 46.7885° |
| argument of perigee: | 315.8835° |
| revolutions per day: | 15.11650048 |
| mean anomaly at epoch: | 44.2322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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