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 63301U 26145.56173146 +.00000000 +00000-0 +22409-3 0 00007
2 63301 97.9065 270.3029 0004460 53.8495 306.3125 14.72393022 05
| Epoch (UTC): | 25 May 2026 13:28:53 |
| Eccentricity: | 0.0004460 |
| inclination: | 97.9065° |
| perigee height: | 650 km |
| apogee height: | 657 km |
| right ascension of ascending node: | 270.3029° |
| argument of perigee: | 53.8495° |
| revolutions per day: | 14.72393022 |
| mean anomaly at epoch: | 306.3125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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