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 63000U 26145.51564903 +.00000000 +00000-0 +53554-3 0 00008
2 63000 43.0028 69.5577 0001382 283.3545 76.7152 15.27595701 01
| Epoch (UTC): | 25 May 2026 12:22:32 |
| Eccentricity: | 0.0001382 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.5577° |
| argument of perigee: | 283.3545° |
| revolutions per day: | 15.27595701 |
| mean anomaly at epoch: | 76.7152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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