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 63060U 26145.64901330 +.00000000 +00000-0 +18504-2 0 00002
2 63060 42.9987 271.5360 0000460 242.8833 117.1987 15.70873795 06
| Epoch (UTC): | 25 May 2026 15:34:34 |
| Eccentricity: | 0.0000460 |
| inclination: | 42.9987° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 271.5360° |
| argument of perigee: | 242.8833° |
| revolutions per day: | 15.70873795 |
| mean anomaly at epoch: | 117.1987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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