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 63368U 26144.96776520 +.00000000 +00000-0 +89403-3 0 00005
2 63368 53.1581 55.6257 0001011 73.5916 286.5196 15.30202419 09
| Epoch (UTC): | 24 May 2026 23:13:34 |
| Eccentricity: | 0.0001011 |
| inclination: | 53.1581° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 55.6257° |
| argument of perigee: | 73.5916° |
| revolutions per day: | 15.30202419 |
| mean anomaly at epoch: | 286.5196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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