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 63303U 26145.60117152 +.00000000 +00000-0 +22101-3 0 00008
2 63303 97.9080 270.2542 0001979 46.0884 314.0487 14.72282673 07
| Epoch (UTC): | 25 May 2026 14:25:41 |
| Eccentricity: | 0.0001979 |
| inclination: | 97.9080° |
| perigee height: | 652 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 270.2542° |
| argument of perigee: | 46.0884° |
| revolutions per day: | 14.72282673 |
| mean anomaly at epoch: | 314.0487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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