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 63373U 26145.15737510 +.00000000 +00000-0 +64872-3 0 00002
2 63373 53.1589 54.6710 0001119 81.0809 279.0319 15.30213216 01
| Epoch (UTC): | 25 May 2026 03:46:37 |
| Eccentricity: | 0.0001119 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 54.6710° |
| argument of perigee: | 81.0809° |
| revolutions per day: | 15.30213216 |
| mean anomaly at epoch: | 279.0319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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