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 63488U 26145.63194130 +.00000000 +00000-0 +67394-3 0 00009
2 63488 97.4851 221.1102 0005818 209.4498 150.6406 15.12283797 09
| Epoch (UTC): | 25 May 2026 15:09:59 |
| Eccentricity: | 0.0005818 |
| inclination: | 97.4851° |
| perigee height: | 525 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 221.1102° |
| argument of perigee: | 209.4498° |
| revolutions per day: | 15.12283797 |
| mean anomaly at epoch: | 150.6406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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