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 63378U 26145.18956030 +.00000000 +00000-0 +65134-3 0 00002
2 63378 53.1576 57.0020 0000891 114.1406 245.9688 15.30218197 04
| Epoch (UTC): | 25 May 2026 04:32:58 |
| Eccentricity: | 0.0000891 |
| inclination: | 53.1576° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 57.0020° |
| argument of perigee: | 114.1406° |
| revolutions per day: | 15.30218197 |
| mean anomaly at epoch: | 245.9688° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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