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 63262U 26145.65414938 +.00000000 +00000-0 +49840-3 0 00008
2 63262 97.6928 39.5411 0006500 88.0151 272.1817 14.99798097 00
| Epoch (UTC): | 25 May 2026 15:41:58 |
| Eccentricity: | 0.0006500 |
| inclination: | 97.6928° |
| perigee height: | 563 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 39.5411° |
| argument of perigee: | 88.0151° |
| revolutions per day: | 14.99798097 |
| mean anomaly at epoch: | 272.1817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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