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 63270U 26145.34719697 +.00000000 +00000-0 +13590-2 0 00005
2 63270 43.0036 10.3493 0004340 268.5046 91.5324 15.70939825 01
| Epoch (UTC): | 25 May 2026 08:19:57 |
| Eccentricity: | 0.0004340 |
| inclination: | 43.0036° |
| perigee height: | 353 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 10.3493° |
| argument of perigee: | 268.5046° |
| revolutions per day: | 15.70939825 |
| mean anomaly at epoch: | 91.5324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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