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 63313U 26145.42322378 +.00000000 +00000-0 +11318-2 0 00004
2 63313 42.9988 162.1970 0000632 223.5413 136.5405 15.70860443 07
| Epoch (UTC): | 25 May 2026 10:09:26 |
| Eccentricity: | 0.0000632 |
| inclination: | 42.9988° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 162.1970° |
| argument of perigee: | 223.5413° |
| revolutions per day: | 15.70860443 |
| mean anomaly at epoch: | 136.5405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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