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 63017U 26145.25958139 +.00000000 +00000-0 +14133-2 0 00004
2 63017 43.0016 94.0335 0002760 257.6105 102.4453 15.70902262 01
| Epoch (UTC): | 25 May 2026 06:13:47 |
| Eccentricity: | 0.0002760 |
| inclination: | 43.0016° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 94.0335° |
| argument of perigee: | 257.6105° |
| revolutions per day: | 15.70902262 |
| mean anomaly at epoch: | 102.4453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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