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 63215U 26145.25322801 +.00000000 +00000-0 +56563-3 0 00009
2 63215 97.3934 41.5575 0003190 145.9761 214.1686 15.33485620 02
| Epoch (UTC): | 25 May 2026 06:04:38 |
| Eccentricity: | 0.0003190 |
| inclination: | 97.3934° |
| perigee height: | 463 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 41.5575° |
| argument of perigee: | 145.9761° |
| revolutions per day: | 15.33485620 |
| mean anomaly at epoch: | 214.1686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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